MINLP in Air Traffic Management: aircraft conflict avoidance
|
|
- Adele Wright
- 6 years ago
- Views:
Transcription
1 MINLP in Air Traffic Management: aircraft conflict avoidance Sonia Cafieri ENAC - École Nationale de l Aviation Civile University of Toulouse France thanks to: Riadh Omheni (ENAC, Toulouse) David Rey (New South Wales, Australia) Second Sevilla Workshop Mixed-Integer Nonlinear Programming Seville, March 30-April 1, 2015 Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
2 Some question... Did you fly to Seville? Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
3 Some question... Did you fly to Seville? Did you think to in-flight safety? How in-flight safety is guaranteed? What does impact it most? Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
4 Air Traffic Management (ATM) & Control ATM : making sure that aicraft are safely guided in the skies and on the ground Air Traffic growing on the world scale Eurocontrol forecast needs increasing automation BOEING long-term market forecast Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
5 Aircraft Conflict Avoidance Aircraft i and j are in conflict if their horizontal distance is less than d: x i (t) x j (t) d t (d = 5NM) their altitude difference is less than h: h i (t) h j (t) h t (h = 1000ft) NM (nautical mile)= 1852 m 1 ft (feet) = m Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
6 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
7 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
8 Aircraft Conflict Avoidance: operational viewpoint Resolution of conflicts currently still largely performed manually by air traffic controllers SESAR & NextGen promote automation projects: Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
9 Aircraft Conflict Avoidance: operational viewpoint Resolution of conflicts currently still largely performed manually by air traffic controllers SESAR & NextGen promote automation projects: Aircraft separation strategies Heading angle deviation Altitude modification Speed adjustements suggested by ERASMUS (En-Route Air Traffic Soft Management Ultimate System) project ( ), allows one to perform a subliminal control Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
10 Aircraft Conflict Avoidance: mathematical/or viewpoint Optimal Control (Tomlin et al. 2004, Cellier et al. 2012) Evolutionary computation (Durand&Alliot 1995, 1998, Delahaye et al. 1996) Mathematical Programming based approaches: Mixed-Integer Linear and Nonlinear Optimization Richards & How, 2002 (MILP) Pallottino, Feron, Bicchi, 2004 (MILP) Christodoulou & Costoulakis, 2004 (MINLP) Vela et al., 2010 (MILP) Alonso-Ayuso, Escudero, Martín-Campo, 2011, 2012, 2013 (MILP, MINLP) Rey et al., 2012 (MILP), 2013 (MINLP) Cafieri & Durand, 2014 (MINLP) Cafieri, 2014 (MINLP) in general, subject to some simplifying hypotesis Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
11 Aircraft Conflict Avoidance: mathematical/or viewpoint Challenge Propose a model corresponding as much as possible to a realistic situation computationally affordable Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
12 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
13 Modeling and optimizing aircraft separation Give a computationally-treatable expression for aircraft separation Choose a separation maneuver decision variables Give a Mathematical Programming formulation for aircraft conflict avoidance Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
14 Modeling and optimizing aircraft separation Give a computationally-treatable expression for aircraft separation Choose a separation maneuver decision variables Give a Mathematical Programming formulation for aircraft conflict avoidance Question: once a separation maneuver (e.g. speed change) is chosen, is the corresponding optimization problem always feasible? combine different separation maneuvers complex models resort to feasibility seeking methods no optimal solution accept that not all conflicts are solved with the selected maneuver and devise suitable pre-processing procedures Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
15 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
16 Aircraft separation Separation condition for aircraft i and j: x r (t) = x i(t) x j (t) d t (0, T) * d = minimum required separation distance * x r (t) = x i(t) x j (t) = x r0 + v r t x r0 v r = relative initial position of aircraft i and j = relative speed of aircraft i and j Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
17 Aircraft separation Separation condition for aircraft i and j: x r (t) = x i(t) x j (t) d t (0, T) depends on t * d = minimum required separation distance * x r (t) = x i(t) x j (t) = x r0 + v r t x r0 v r = relative initial position of aircraft i and j = relative speed of aircraft i and j i.e. x r0 + v r t 2 d 2 t (0, T) v r 2 t 2 + 2(x r0 vr ) t + ( xr0 2 d 2 ) 0 Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
18 Aircraft separation 1) By differentiation, compute the minimizer t m = ( ) x r0 v r / v r 2 and substitute: x r0 2 (xr0 v r )2 v r d Separation: if t m > 0 then condition x r0 2 (xr0 v r )2 v r d Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
19 Aircraft separation 1) By differentiation, compute the minimizer t m = ( ) x r0 v r / v r 2 and substitute: x r0 2 (xr0 v r )2 v r d 2 0 does not depend on t 2 Separation: if t m > 0 then condition x r0 2 (xr0 v r )2 v r d ) Compute the discriminant: = (x r0 v r )2 v r 2 ( x r0 2 d 2 ) does not depend on t Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
20 Aircraft separation 1) By differentiation, compute the minimizer t m = ( ) x r0 v r / v r 2 and substitute: x r0 2 (xr0 v r )2 v r d Separation: if t m > 0 then condition x r0 2 (xr0 v r )2 v r d ) Compute the discriminant: = (x r0 v r )2 v r 2 ( x r0 2 d 2 ) Separation: 2.1) 0 no solutions, aircraft separated 2.2) > 0 and both roots t, t negative t = 2(xr0 v r ) 2 v r and t = 2(xr0 v r ) v r 2 Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
21 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
22 Maximizing solved conflicts by speed regulation separation maneuver selection = Separation based on speed regulation using subliminal control How many conflicts can be solved using the selected maneuver? Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
23 Maximizing solved conflicts by speed regulation separation maneuver selection = Separation based on speed regulation using subliminal control How many conflicts can be solved using the selected maneuver? Maximize the number of conflits that are solved by speed regulation discriminate between conflicts that can be solved by speed changes and those needing other maneuvers may be used as a pre-processing for another model Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
24 MINLP formulation: Max VC (1/4) A = set of n aircraft Variables: { 1 if i and j are separated (no conflict) i, j A, i < j z = 0 otherwise v i, v min, v max i A, aircraft speeds (continuous) speed change between -6% and +3% of the original speed subliminal control i, j A, auxiliary var. for the inner product x r0 v r (continuous) Objective: maximize the number of solved conflicts: max i,j A, i<j z Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
25 MINLP formulation: Max VC (2/4) Constraints: integrality constraints on z variables bounds on v variables separation constraints on pairs of aircraft Separation constraints: count the number of aircraft pairs for which 0 (condition 2.1) ( (x r0 v r )2 v r 2 ( x r0 2 d 2 ) ) (2 z 1) 0 i, j A, i < j Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
26 MINLP formulation: Max VC (3/4) Pairs of separated aircraft may potentially be not counted couple the -based condition with a simple geometric condition - Assume that trajectories are straight lines intersecting in one point - look at the sign of the scalar product x r0 v r Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
27 MINLP formulation: Max VC (3/4) Pairs of separated aircraft may potentially be not counted couple the -based condition with a simple geometric condition If x r0 v r 0 aircraft diverging separated if separated at their initial positions 0 OR x r0 v r 0 aircraft separated Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
28 MINLP formulation: Max VC (3/4) Pairs of separated aircraft may potentially be not counted couple the -based condition with a simple geometric condition If x r0 v r 0 aircraft diverging separated if separated at their initial positions 0 OR x r0 v r 0 aircraft separated Separation constraints: (x r0 v r )2 (2 z 1) v r 2 ( x r0 2 d 2 ) (2 z 1) OR (x r0 v r ) (2 y 1) 0 i, j A, i < j i, j A, i < j Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
29 MINLP formulation: Max VC (4/4) Modeling the OR condition: use an additional variable 0 w 1, i, j, i < j Separation constraints: (x r0 v r )2 (2 z 1) v r 2 ( x r0 2 d 2 ) (2 z 1) (x r0 v r ) (2 y 1) 0 w z w y w z + y i, j A, i < j i, j A, i < j i, j A, i < j i, j A, i < j i, j A, i < j and maximize max i,j A, i<j w Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
30 Numerical results Test problems Solution approach Global solution spatial Branch-and-Bound COUENNE 0.4 (Belotti et al., 2008) AMPL model conflict zone n aircraft n {1,..., 6} aircraft n(n 1)/2 conflicts d = 5 NM, v = 400 NM/h Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
31 Numerical solution Max VC n radius n confl obj time (s) pb_n pb_n pb_n pb_n pb_n CP_n CP_n Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
32 Numerical solution Max VC n radius n confl obj time (s) pb_n pb_n pb_n pb_n pb_n CP_n CP_n promising results; not guaranteed solving all conflicts Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
33 Numerical solution Max VC n radius n confl obj time (s) pb_n pb_n pb_n pb_n pb_n CP_n CP_n Example pb_n5, n = 5 (10 conflicts) aircraft v ratio = v/ v aircraft accelerated, 3 decelerated speed variations in [-6%, +3%] around the original velocity (subliminal control) Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
34 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
35 Solving all conflicts with Riadh Omheni (ENAC, Toulouse) If not all conflicts are solved by speed changes Solve conflicts by heading angle changes = new model using the first one as a pre-processing step speed changes + heading angle changes Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
36 Solving all conflicts with Riadh Omheni (ENAC, Toulouse) If not all conflicts are solved by speed changes Solve conflicts by heading angle changes = new model using the first one as a pre-processing step speed changes + heading angle changes Algorithm Input: n, A maximize the number of solved conflicts by speed regulation if (there are still unsolved conflicts) then solve conflicts by heading angle changes minimizing angle deviations endif Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
37 Solving conflicts by heading angle changes (HAC) Recall separation (condition 1): if t m > 0 then x r0 2 (xr0 v r )2 v r d Relative velocity vector: v r = cos(φ i )v i cos(φ j )v j sin(φ i )v i sin(φ j )v j Changing heading angle changing Φ = φ + θ v r = cos(φ i + θ i )v i cos(φ j + θ j )v j sin(φ i + θ i )v i sin(φ j + θ j )v j with θ bounded and v i, v j kept unchanged. Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
38 MINLP formulation: HAC (1/3) Variables: θ i, ( θ min, θ max ), i A angle variation of aircraft i (continuous) v 2r, (i, j) A, i < j square of the relative velocity of i and j (continuous) p, (i, j) A, i < j t m, (i, j) A, i < j (continuous) inner product v r xr0 (continuous) y, (i, j) A, i < j, used to check if t m > 0 (binary) Objective: min i A θ 2 i minimizing angle deviations Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
39 MINLP formulation: HAC (2/3) Constraints: definition of v 2r (quadratic, trigonometric functions) v 2r = ( v i cos(φ i + θ i ) v j cos(φ j + θ j ) ) 2 + ( v i sin(φ i + θ i ) v j sin(φ j + θ j ) ) 2 i, j A, i < j inner product in the separation condition (trigonometric functions) p = (x 0 i,1 x0 j,1 ) ( v i cos(φ i + θ i ) v j cos(φ j + θ j ) ) + (x 0 i,2 x0 j,2 ) ( v i sin(φ i + θ i ) v j sin(φ j + θ j ) ) i, j A, i < j definition of t m check sign of t m (bilinear) t m v2r + p = 0 (i, j) A, i < j (bilinear with binary var.) t m (2y 1) 0 (i, j) A, i < j separation (quadratic + linear term, product with binary var.) y ( (x 0r v2r ) (p ) 2 ((d) 2 v 2r )) 0 (i, j) A, i < j Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
40 MINLP: HAC reformulation (3/3) Compute bounds on variables v r, p and t m ( obtain (t m ) min, (t m ) max) Reformulate products of binary variables y reformulate t m (2y 1) 0 and continuous variables (i, j) A, i < j to t m i,j (t m ) min (1 y ) (i, j) A, i < j t m i,j (t m ) max y reformulate y ( (x 0r v2r ) (p ) 2 ((d) 2 v 2r )) 0 (i, j) A, i < j to (x 0r d 2 ) v 2r (p ) 2 bigm (1 y ) (i, j) A, i < j Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
41 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
42 Numerical results: HAC HAC n n c nrc time (s) obj pb-hth_n pb-hth_n pb-hth_n pb-hth_n CP_n CP_n CP full _n CP full _n CP half _n CP half _n RCP full _n RCP full _n promising computing time - exact solution Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
43 Numerical results: HAC Example: n = 3 aircraft, 1 head-to-head Φ j Φ i Φ k Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
44 Numerical results: HAC Example: n = 3 aircraft, 1 head-to-head Φ j Φ j Θ j Θ i Φ i Φ k Φ i Θ k = 0 Φ k Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
45 Numerical results: Max VC + HAC Max VC n n c nrc time (s) pb-hth_n pb-hth_n pb-hth_n pb-hth_n CP_n CP_n CP full _n CP full _n CP half _n CP half _n RCP full _n RCP full _n Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
46 Numerical results: Max VC + HAC Max VC HAC n n c (pre-processing) (with pre-processing) n rc time (s) n rc time (s) obj pb-hth_n pb-hth_n pb-hth_n pb-hth_n CP_n CP_n CP full _n CP full _n CP half _n CP half _n RCP full _n RCP full _n Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
47 Numerical results: Max VC + HAC Max VC HAC HAC n n c (pre-processing) (with pre-processing) n rc time (s) n rc time (s) obj n rc time (s) obj pb-hth_n pb-hth_n pb-hth_n pb-hth_n CP_n CP_n CP full _n CP full _n CP half _n CP half _n RCP full _n RCP full _n pre-processing reduces, sometimes significantly, computing time Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
48 Numerical results: Max VC + HAC Max VC HAC HAC n n c (pre-processing) (with pre-processing) n rc time (s) n rc time (s) obj n rc time (s) obj pb-hth_n pb-hth_n pb-hth_n pb-hth_n CP_n CP_n CP full _n CP full _n CP half _n CP half _n RCP full _n RCP full _n pre-processing reduces, sometimes significantly, computing time Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
49 Outline 1 Conflict Avoidance in ATM: background 2 MINLP models Aircraft separation modeling Maximizing the number of solved conflicts by speed regulation Solving conflicts by heading angle changes 3 Numerical results 4 Conclusions and Perspectives Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
50 Conclusions and Perspectives Promising results combining two MINLP models based on different maneuvers to separate aircraft MINLP model for maximizing the number of solved aircraft conflicts: helps filtering conflicts with respect to the selected separation maneuver Future work: decomposition-based approaches with D. Rey (New South Wales, Australia) solution by Interval Branch&Bound techniques with F. Messine (Toulouse, France) ATOMIC = Air Traffic Optimization by Mixed-Integer Computation project funded by French National Agency of Research Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
51 The end Thank you! Sonia Cafieri (ENAC) MINLP in Air Traffic Management Seville, / 36
Mixed-Integer Nonlinear Programming for Aircraft Conflict Avoidance by Sequentially Applying Velocity and Heading Angle Changes
Mixed-Integer Nonlinear Programming for Aircraft Conflict Avoidance by Sequentially Applying Velocity and Heading Angle Changes Sonia Cafieri, Riadh Omheni To cite this version: Sonia Cafieri, Riadh Omheni.
More informationMINLP in Air Traffic Management: Aircraft Conflict Avoidance
MINLP in Air Traffic Management: Aircraft Conflict Avoidance Sonia Cafieri To cite this version: Sonia Cafieri. MINLP in Air Traffic Management: Aircraft Conflict Avoidance. Edited by Tamás Terlaky, Miguel
More informationOn Solving Aircraft Conflict Avoidance Using Deterministic Global Optimization (sbb) Codes
On Solving Aircraft Conflict Avoidance Using Deterministic Global Optimization (sbb) Codes Sonia Cafieri, Frédéric Messine, Ahmed Touhami To cite this version: Sonia Cafieri, Frédéric Messine, Ahmed Touhami.
More informationFeasibility pump for aircraft deconfliction with speed regulation
Feasibility pump for aircraft deconfliction with speed regulation Sonia Cafieri, Claudia D Ambrosio To cite this version: Sonia Cafieri, Claudia D Ambrosio. Feasibility pump for aircraft deconfliction
More informationComplex Number Formulation and Convex Relaxations for Aircraft Conflict Resolution
Complex Number Formulation and Convex Relaxations for Aircraft Conflict Resolution David Rey and Hassan Hijazi Abstract We present a novel complex number formulation along with tight convex relaxations
More informationA New Framework for Solving En-Route Conflicts
A New Framework for Solving En-Route Conflicts Cyril Allignol, Nicolas Barnier, Nicolas Durand and Jean-Marc Alliot allignol,barnier,durand@recherche.enac.fr jean-marc.alliot@irit.fr ATM 2013 Chicago June
More informationThe Influence of Uncertainties on TCSA
The Influence of Uncertainties on TCSA Géraud Granger, Cyril Allignol, Nicolas Durand DSNA/R&D http://pom.tls.cena.fr/pom June 14, 2011 Introduction The CATS/ERCOS Simulator Simulation Results Conclusion
More informationLarge-Scale 3D En-Route Conflict Resolution
Large-Scale 3D En-Route Conflict Resolution Cyril Allignol, Nicolas Barnier, Nicolas Durand, Alexandre Gondran and Ruixin Wang allignol,barnier,durand,gondran,wangrx @recherche.enac.fr ATM 2017 Seattle
More informationThe Influence of Uncertainties on Traffic Control using Speed Adjustments
NINTH USA/EUROPE AIR TRAFFIC MANAGEMENT RESEARCH AND DEVELOPMENT SEMINAR (ATM2011) 1 The Influence of Uncertainties on Traffic Control using Speed Adjustments Géraud Granger STERIA 7, av Edouard Belin
More informationComplexity Metrics. ICRAT Tutorial on Airborne self separation in air transportation Budapest, Hungary June 1, 2010.
Complexity Metrics ICRAT Tutorial on Airborne self separation in air transportation Budapest, Hungary June 1, 2010 Outline Introduction and motivation The notion of air traffic complexity Relevant characteristics
More informationSAFETY AND CONVERGENCE ANALYSIS OF INTERSECTING AIRCRAFT FLOWS UNDER DECENTRALIZED COLLISION AVOIDANCE
SAFETY AND CONVERGENCE ANALYSIS OF INTERSECTING AIRCRAFT FLOWS UNDER DECENTRALIZED COLLISION AVOIDANCE by Ahmed H. Dallal B.S. in Biomedical Engineering, Cairo University, 2009 M.S. in Biomedical Engineering,
More informationProgramming (MIP) problem, which may be solved using optimization tools such as CPLEX [1]. The simplicity of the model with respect to the nonlinear m
1 Conflict Resolution Problems f Air Traffic Management Systems Solved with Mixed Integer Programming Lucia Pallottino, Eric Feron, Antonio Bicchi Keywds Mixed Integer Programming, Air Traffic Management
More informationIndicator Constraints in Mixed-Integer Programming
Indicator Constraints in Mixed-Integer Programming Andrea Lodi University of Bologna, Italy - andrea.lodi@unibo.it Amaya Nogales-Gómez, Universidad de Sevilla, Spain Pietro Belotti, FICO, UK Matteo Fischetti,
More informationDevelopment of an algorithm for solving mixed integer and nonconvex problems arising in electrical supply networks
Development of an algorithm for solving mixed integer and nonconvex problems arising in electrical supply networks E. Wanufelle 1 S. Leyffer 2 A. Sartenaer 1 Ph. Toint 1 1 FUNDP, University of Namur 2
More informationAnalytical Workload Model for Estimating En Route Sector Capacity in Convective Weather*
Analytical Workload Model for Estimating En Route Sector Capacity in Convective Weather* John Cho, Jerry Welch, and Ngaire Underhill 16 June 2011 Paper 33-1 *This work was sponsored by the Federal Aviation
More informationProvably Safe Coordinated Strategy for Distributed Conflict Resolution
AIAA Guidance, Navigation, and Control Conference and Exhibit 5-8 August 2005, San Francisco, California AIAA 2005-6047 Provably Safe Coordinated Strategy for Distributed Conflict Resolution Gilles Dowek
More informationGeometric and probabilistic approaches towards Conflict Prediction
Geometric and probabilistic approaches towards Conflict Prediction G.J. Bakker, H.J. Kremer and H.A.P. Blom Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory NLR Geometric and probabilistic
More informationReach Sets and the Hamilton-Jacobi Equation
Reach Sets and the Hamilton-Jacobi Equation Ian Mitchell Department of Computer Science The University of British Columbia Joint work with Alex Bayen, Meeko Oishi & Claire Tomlin (Stanford) research supported
More informationTHIS PAPER addresses the decoupling of conflictresolution
422 IEEE TRANSACTIONS ON INTELLIGENT TRANSPORTATION SYSTEMS, VOL. 12, NO. 2, JUNE 2011 Decoupled Conflict-Resolution Procedures for Decentralized Air Traffic Control Santosh Devasia, Dhanakorn Iamratanakul,
More informationTIME OPTIMAL MANAGEMENT BY SEVERAL AIRCRAFT FLOWS IN POINT-MERGE SCHEMES 1
TIME OPTIMAL MANAGEMENT BY SEVERAL AIRCRAFT FLOWS IN POINT-MERGE SCHEMES 1 S.I. Kumkov, S.G. Pyatko, M.M. Ovchinnikov World ATM Congress 2016 Madrid, Spain, March 08 10, 2016 The Frequentis Aviation Arena
More informationA Branch-and-Refine Method for Nonconvex Mixed-Integer Optimization
A Branch-and-Refine Method for Nonconvex Mixed-Integer Optimization Sven Leyffer 2 Annick Sartenaer 1 Emilie Wanufelle 1 1 University of Namur, Belgium 2 Argonne National Laboratory, USA IMA Workshop,
More informationDecentralized Cooperative Conflict Resolution Among Multiple Autonomous Mobile Agents
Decentralized Cooperative Conflict Resolution Among Multiple Autonomous Mobile Agents Lucia Pallottino, Vincenzo Giovanni Scordio, Antonio Bicchi Abstract In this paper we consider policies for cooperative,
More information[EN-A-083] Potential Benefits of Speed Control on Delay and Fuel Consumption
ENRI Int. Workshop on ATM/CNS. Tokyo, Japan. (EIWAC 2017) [EN-A-083] Potential Benefits of Speed Control on Delay and Fuel Consumption (EIWAC 2017) + Y. Matsuno*, A. Andreeva-Mori*, T. Uemura*, N. Matayoshi*
More informationJoint Metering and Conflict Resolution in Air Traffic Control
University of Pennsylvania ScholarlyCommons Technical Reports (ESE) Department of Electrical & Systems Engineering -28-200 Joint Metering and Conflict Resolution in Air Traffic Control Jerome Le Ny University
More informationEvolving Meteorological Services for the Terminal Area
Evolving Meteorological Services for the Terminal Area Towards an new participatory approach in ATM H. Puempel Chief, Aeronautical Meteorology Division Weather and Disaster Risk Reduction Dept. WMO The
More informationA Novel Framework to Assess the Wake Vortex Hazards Risk Supported by Aircraft in En Route Operations
R WAKE SESAR 2020 Exploratory Research Project A Novel Framework to Assess the Wake Vortex Hazards Risk Supported by Aircraft in En Route Operations Marc Melgosa and Xavier Prats Department of Physics
More informationSolving Mixed-Integer Nonlinear Programs
Solving Mixed-Integer Nonlinear Programs (with SCIP) Ambros M. Gleixner Zuse Institute Berlin MATHEON Berlin Mathematical School 5th Porto Meeting on Mathematics for Industry, April 10 11, 2014, Porto
More informationA Bayesian. Network Model of Pilot Response to TCAS RAs. MIT Lincoln Laboratory. Robert Moss & Ted Londner. Federal Aviation Administration
A Bayesian Network Model of Pilot Response to TCAS RAs Robert Moss & Ted Londner MIT Lincoln Laboratory ATM R&D Seminar June 28, 2017 This work is sponsored by the under Air Force Contract #FA8721-05-C-0002.
More informationMixed-Integer Nonlinear Programming
Mixed-Integer Nonlinear Programming Claudia D Ambrosio CNRS researcher LIX, École Polytechnique, France pictures taken from slides by Leo Liberti MPRO PMA 2016-2017 Motivating Applications Nonlinear Knapsack
More informationCHAPTER 3: INTEGER PROGRAMMING
CHAPTER 3: INTEGER PROGRAMMING Overview To this point, we have considered optimization problems with continuous design variables. That is, the design variables can take any value within a continuous feasible
More informationAircraft Trajectory Planning With Collision Avoidance Using Mixed Integer Linear Programming
Proceedings of the American Control Conference Anchorage, AK May 8-10,2002 Aircraft Trajectory Planning With Collision Avoidance Using Mixed Integer Linear Programming Arthur Richards and Jonathan P. How
More informationOptimal Scheduling Algorithm in Point Merge System Including Holding Pattern Based on MILP
7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Optimal Scheduling Algorithm in Point Merge System Including Holding Pattern Based on MILP Somang Lee, Youkyung Hong, and Youdan
More informationFederal Aviation Administration Optimal Aircraft Rerouting During Commercial Space Launches
Federal Aviation Administration Optimal Aircraft Rerouting During Commercial Space Launches Rachael Tompa Mykel Kochenderfer Stanford University Oct 28, 2015 1 Motivation! Problem: Launch vehicle anomaly
More informationCONFLICT RESOLUTION AND TRAFFIC COMPLEXITY OF MULTIPLE INTERSECTING FLOWS OF AIRCRAFT
CONFLICT RESOLUTION AND TRAFFIC COMPLEXITY OF MULTIPLE INTERSECTING FLOWS OF AIRCRAFT by Kyle Treleaven B.S. in Electrical Engineering, University of Pittsburgh, 2006 Submitted to the Graduate Faculty
More informationGraceful Degradation of Air Traffic Operations
1 Graceful Degradation of Air Traffic Operations Maxime Gariel and Eric Feron Georgia Institute of Technology Atlanta, GA, 3033-0150, USA arxiv:0801.4750v1 [cs.oh] 30 Jan 008 Abstract The introduction
More informationDevelopment of a new method for ATFCM based on trajectory based operations
Original Article Development of a new method for ATFCM based on trajectory based operations Dany Gatsinzi, Francisco J Saez Nieto, Irfan Madani Abstract This paper discusses a possibility to evolve the
More informationMixed Integer Non Linear Programming
Mixed Integer Non Linear Programming Claudia D Ambrosio CNRS Research Scientist CNRS & LIX, École Polytechnique MPRO PMA 2016-2017 Outline What is a MINLP? Dealing with nonconvexities Global Optimization
More informationHIGH DENSITY EN ROUTE AIRSPACE SAFETY LEVEL AND COLLISION RISK ESTIMATION BASED ON STORED AIRCRAFT TRACKS
HIGH DENSITY EN ROUTE AIRSPACE SAFETY LEVEL AND COLLISION RISK ESTIMATION BASED ON STORED AIRCRAFT TRACKS (EIWAC 2010) + E. Garcia*, F. Saez**, R. Arnaldo** * CRIDA (ATM Research, Development and Innovation
More informationTraffic Flow Management (TFM) Weather Rerouting Decision Support. Stephen Zobell, Celesta Ball, and Joseph Sherry MITRE/CAASD, McLean, Virginia
Traffic Flow Management (TFM) Weather Rerouting Decision Support Stephen Zobell, Celesta Ball, and Joseph Sherry MITRE/CAASD, McLean, Virginia Stephen Zobell, Celesta Ball, and Joseph Sherry are Technical
More informationLinear programming: algebra
: algebra CE 377K March 26, 2015 ANNOUNCEMENTS Groups and project topics due soon Announcements Groups and project topics due soon Did everyone get my test email? Announcements REVIEW geometry Review geometry
More informationA DISPLAY CONCEPT FOR STAYING AHEAD OF THE AIRPLANE
A DISPLAY CONCEPT FOR STAYING AHEAD OF THE AIRPLANE Eric N. Johnson, Lockheed Martin Aeronautical Systems, Marietta, Georgia David C. Hansen, Lockheed Martin Aeronautical Systems, Marietta, Georgia Abstract
More informationVelocity Tuning for Air Traffic Control
Velocity Tuning for Air Traffic Control Sander van der Hurk Supervisors: prof. dr. M.J. van Kreveld dr. ir. A.F. van der Stappen June 19, 2015 Abstract In this thesis we study air traffic conflict resolution
More informationRelaxations of multilinear convex envelopes: dual is better than primal
of multilinear convex envelopes: dual is better than primal 1 LIX, École Polytechnique, Palaiseau, France June 7th, 2012 11 th International Symposium on Experimental Algorithms (SEA) 2012 - Bordeaux (France)
More informationSOLUTIONS FOR PROBLEMS 1-30
. Answer: 5 Evaluate x x + 9 for x SOLUTIONS FOR PROBLEMS - 0 When substituting x in x be sure to do the exponent before the multiplication by to get (). + 9 5 + When multiplying ( ) so that ( 7) ( ).
More informationWeather in the Connected Cockpit
Weather in the Connected Cockpit What if the Cockpit is on the Ground? The Weather Story for UAS Friends and Partners of Aviation Weather November 2, 2016 Chris Brinton brinton@mosaicatm.com Outline Mosaic
More informationDESIGN OF FLIGHT AVOIDANCE MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT
DESIGN OF FLIGHT AVOIDANCE MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT Onvaree Techakesari, Jason J. Ford, Paul M. Zapotezny-Anderson Australian Research Centre for Aerospace
More informationI. Introduction. external compression. supersonic flow. II. Design Criteria
Design Optimization of High Speed Inlets Doyle D Knight Dept of Mechanical and Aerospace Engineering Rutgers - The State University of New Jersey New Brunswick, NJ 08903 knight@soemailrutgersedu I Introduction
More information4D TRAJECTORY BASED OPERATION IN HIGH DENSITY TERMINAL CONTROL AREA CONSIDERING THE UNCERTAINTY OF WEATHER FORECAST DATA
4D TRAJECTORY BASED OPERATION IN HIGH DENSITY TERMINAL CONTROL AREA CONSIDERING THE UNCERTAINTY OF WEATHER FORECAST DATA Asei Tezuka Waseda University Keywords: Aircraft Trajectory Prediction, Meteorological
More informationBasic notions of Mixed Integer Non-Linear Programming
Basic notions of Mixed Integer Non-Linear Programming Claudia D Ambrosio CNRS & LIX, École Polytechnique 5th Porto Meeting on Mathematics for Industry, April 10, 2014 C. D Ambrosio (CNRS) April 10, 2014
More informationSelected Examples of CONIC DUALITY AT WORK Robust Linear Optimization Synthesis of Linear Controllers Matrix Cube Theorem A.
. Selected Examples of CONIC DUALITY AT WORK Robust Linear Optimization Synthesis of Linear Controllers Matrix Cube Theorem A. Nemirovski Arkadi.Nemirovski@isye.gatech.edu Linear Optimization Problem,
More informationTRAJECTORY PREDICTION UNCERTAINTY MODELING FOR CONTINUOUS DESCENT APPROACHES
27 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES TRAJECTORY PREDICTION UNCERTAINTY MODELING FOR CONTINUOUS DESCENT APPROACHES Gabriele Enea*, Robert Vivona*, David Karr*, Karen Cate** *Engility
More informationTHIS BRIEF presents a procedure for resolving conflicts
2280 IEEE TANSACTIONS ON CONTOL SYSTEMS TECHNOLOGY, VOL. 21, NO. 6, NOVEMBE 2013 Provably Safe Conflict esolution With Bounded Turn ate for Air Traffic Control Jeff Yoo and Santosh evasia Abstract This
More informationA Hierarchical Model-based Optimization Control Method for Merging of Connected Automated Vehicles. Na Chen, Meng Wang, Tom Alkim, Bart van Arem
A Hierarchical Model-based Optimization Control Method for Merging of Connected Automated Vehicles Na Chen, Meng Wang, Tom Alkim, Bart van Arem 1 Background Vehicle-to-Vehicle communication Vehicle-to-Infrastructure
More informationANALYSIS OF AIRCRAFT LATERAL PATH TRACKING ACCURACY AND ITS IMPLICATIONS FOR SEPARATION STANDARDS
ANALYSIS OF AIRCRAFT LATERAL PATH TRACKING ACCURACY AND ITS IMPLICATIONS FOR SEPARATION STANDARDS Michael Cramer, The MITRE Corporation, McLean, VA Laura Rodriguez, The MITRE Corporation, McLean, VA Abstract
More informationA Case Study of Non-linear Dynamics of Human-Flow Behavior in Terminal Airspace
A Case Study of Non-linear Dynamics of Human-Flow Behavior in Terminal Airspace Lei Yang a,b, Suwan Yin a,b, Minghua Hu a,b, Yan Xu c a Nanjing University of Aeronautics and Astronautics b National Lab
More informationOn mathematical programming with indicator constraints
On mathematical programming with indicator constraints Andrea Lodi joint work with P. Bonami & A. Tramontani (IBM), S. Wiese (Unibo) University of Bologna, Italy École Polytechnique de Montréal, Québec,
More informationAdvanced Aircraft Performance Modeling for ATM: Enhancements to the BADA Model
Advanced Aircraft Performance Modeling for ATM: Enhancements to the BADA Model Presented at 24 th Digital Avionics System Conference Washington D.C. October 30 November 3, 2005 Angela Nuic, Chantal Poinsot,
More informationSoftware for Integer and Nonlinear Optimization
Software for Integer and Nonlinear Optimization Sven Leyffer, leyffer@mcs.anl.gov Mathematics & Computer Science Division Argonne National Laboratory Roger Fletcher & Jeff Linderoth Advanced Methods and
More informationVectors are used to represent quantities such as force and velocity which have both. and. The magnitude of a vector corresponds to its.
Fry Texas A&M University Fall 2016 Math 150 Notes Chapter 9 Page 248 Chapter 9 -- Vectors Remember that is the set of real numbers, often represented by the number line, 2 is the notation for the 2-dimensional
More informationCSCI 1951-G Optimization Methods in Finance Part 10: Conic Optimization
CSCI 1951-G Optimization Methods in Finance Part 10: Conic Optimization April 6, 2018 1 / 34 This material is covered in the textbook, Chapters 9 and 10. Some of the materials are taken from it. Some of
More informationOPTIMIZATION. joint course with. Ottimizzazione Discreta and Complementi di R.O. Edoardo Amaldi. DEIB Politecnico di Milano
OPTIMIZATION joint course with Ottimizzazione Discreta and Complementi di R.O. Edoardo Amaldi DEIB Politecnico di Milano edoardo.amaldi@polimi.it Website: http://home.deib.polimi.it/amaldi/opt-15-16.shtml
More informationMode-S EHS data usage in the meteorological domain:
Mode-S EHS data usage in the meteorological domain: derivation of Wind and Temperature observations; and assimilation of these observations in a numerical weather prediction model. Jan Sondij, MBA Senior
More informationRoute-Planning for Real-Time Safety-Assured Autonomous Aircraft (RTS3A)
Route-Planning for Real-Time Safety-Assured Autonomous Aircraft (RTS3A) Raghvendra V. Cowlagi 1 Jeffrey T. Chambers 2 Nikola Baltadjiev 2 1 Worcester Polytechnic Institute, Worcester, MA. 2 Aurora Flight
More informationA Sufficient Comparison of Trackers
A Sufficient Comparison of Trackers David Bizup University of Virginia Department of Systems and Information Engineering P.O. Box 400747 151 Engineer's Way Charlottesville, VA 22904 Donald E. Brown University
More informationNew trends in Air Traffic Complexity
New trends in Air Traffic Complexity D. Delahaye and S. Puechmorel Applied Math Laboratory, ENAC March 8, 2010 D. Delahaye and S. Puechmorel (Applied Math Laboratory, New trends ENAC) in Air Traffic Complexity
More informationFuture Aeronautical Meteorology Research & Development
Future Aeronautical Meteorology Research & Development Matthias Steiner National Center for Atmospheric Research (NCAR) Boulder, Colorado, USA msteiner@ucar.edu WMO Aeronautical Meteorology Scientific
More informationMulti-objective optimization of workload to study the locus of control in a novel airspace
Multi-objective optimization of workload to study the locus of control in a novel airspace KENN C. NELSON Department of pplied Mathematics and Statistics University of California, Santa Cruz ugust 2, 2015
More informationMILP reformulation of the multi-echelon stochastic inventory system with uncertain demands
MILP reformulation of the multi-echelon stochastic inventory system with uncertain demands Axel Nyberg Åbo Aademi University Ignacio E. Grossmann Dept. of Chemical Engineering, Carnegie Mellon University,
More informationA Fast Heuristic for GO and MINLP
A Fast Heuristic for GO and MINLP John W. Chinneck, M. Shafique, Systems and Computer Engineering Carleton University, Ottawa, Canada Introduction Goal: Find a good quality GO/MINLP solution quickly. Trade
More informationOptimal Maneuver for Multiple Aircraft Conflict Resolution: A Braid Point of View 1
Optimal Maneuver for Multiple Aircraft Conflict Resolution: A Braid Point of View 1 Jianghai Hu jianghai@eecs.berkeley.edu Electrical Eng. & Comp. Science Univ. of California at Berkeley Maria Prandini
More informationA Market Mechanism to Assign Air Traffic Flow Management Slots
A Market Mechanism to Assign Air Traffic Flow Management Slots Andrea Ranieri, Lorenzo Castelli Università degli Studi di Trieste Dipartimento di Elettrotecnica, Elettronica ed Informatica 8 th USA/Europe
More informationAir Traffic Complexity Resolution in Multi-Sector Planning
Air Resolution in Multi-Sector Planning Using CP Pierre Flener 1 Justin Pearson 1 Magnus Ågren 1 Carlos Garcia-Avello 2 Mete Çeliktin 2 Søren Dissing 2 1 Department of Information Technology, Uppsala University,
More informationAviation Weather. Segment Three - Concept of Operations and Requirements. Federal Aviation Administration
Aviation Weather Segment Three - Concept of Operations and Requirements Presented to: Panel: Friends/Partners in Aviation Weather Vision Forum Richard Heuwinkel, Kevin Johnston, Leo Prusak, and Joe Sherry
More informationThe fire and rescue vehicle location problem
The fire and rescue vehicle location problem Henrik Andersson Norwegian University of Science and Technology Tobias Andersson Granberg Linköping University Introduction The Swedish Civil Contingencies
More informationFeasibility Investigation on Reduced-Power Take-off of MA600
Advanced Materials Research Online: 2013-09-04 ISSN: 1662-8985, Vols. 779-780, pp 486-490 doi:10.4028/www.scientific.net/amr.779-780.486 2013 Trans Tech Publications, Switzerland Feasibility Investigation
More informationTo teach the instrument student knowledge of the elements related to an instrument takeoff and the primary instruments for pitch, bank, and power.
INSTRMENT TAKEOFF (1.1..) OBJECTIVE To teach the instrument student knowledge of the elements related to an instrument takeoff and the primary instruments for pitch, bank, and power. COMPLETION STANDARDS
More informationMixed Integer Programming Solvers: from Where to Where. Andrea Lodi University of Bologna, Italy
Mixed Integer Programming Solvers: from Where to Where Andrea Lodi University of Bologna, Italy andrea.lodi@unibo.it November 30, 2011 @ Explanatory Workshop on Locational Analysis, Sevilla A. Lodi, MIP
More informationMachine learning, ALAMO, and constrained regression
Machine learning, ALAMO, and constrained regression Nick Sahinidis Acknowledgments: Alison Cozad, David Miller, Zach Wilson MACHINE LEARNING PROBLEM Build a model of output variables as a function of input
More informationMathematical Techniques for Pre-conceptual Design
Mathematical Techniques for Pre-conceptual Design Mathematical Modeling in Industry XI IMA University of Minnesota Mentor: John Hoffman, Lockheed Martin Tactical Systems Michael Case 1, Jeff Haack 2, MoonChang
More informationOptimization-based Modeling and Analysis Techniques for Safety-Critical Software Verification
Optimization-based Modeling and Analysis Techniques for Safety-Critical Software Verification Mardavij Roozbehani Eric Feron Laboratory for Information and Decision Systems Department of Aeronautics and
More informationWMO Aviation Research Demonstration Project (AvRDP) and Seamless Trajectory Based Operation (TBO) PW Peter Li
WMO Aviation Research Demonstration Project (AvRDP) and Seamless Trajectory Based Operation (TBO) PW Peter Li Hong Kong Observatory Chair, AvRDP SSC New Era of Aviation Industry WMO Congress XVI recognized
More informationSemi-decidable Synthesis for Triangular Hybrid Systems
Semi-decidable Synthesis for Triangular Hybrid Systems Omid Shakernia 1, George J. Pappas 2, and Shankar Sastry 1 1 Department of EECS, University of California at Berkeley, Berkeley, CA 94704 {omids,sastry}@eecs.berkeley.edu
More informationA statistical analysis of the influence of vertical and ground speed errors on conflict probe
A statistical analysis of the influence of vertical and ground speed errors on conflict probe Jean-Marc Alliot Nicolas urand Géraud Granger CENA CENA CENA Keyords: air traffic control, conflict probe,
More information6th USA/Europe ATM 2005 R&D Seminar Statistical performance evaluation between linear and nonlinear designs for aircraft relative guidance
direction des services de la Navigation aérienne direction de la Technique et de Presented by Thierry MIQUE 6th USA/Europe ATM 005 R&D Seminar Statistical performance evaluation between linear and nonlinear
More information1.1 ATM-WEATHER INTEGRATION AND TRANSLATION MODEL. Steve Bradford, David J. Pace Federal Aviation Administration, Washington, DC
1.1 ATM-WEATHER INTEGRATION AND TRANSLATION MODEL Steve Bradford, David J. Pace Federal Aviation Administration, Washington, DC Matt Fronzak *, Mark Huberdeau, Claudia McKnight, Gene Wilhelm The MITRE
More informationHigher Mathematics Skills Checklist
Higher Mathematics Skills Checklist 1.1 The Straight Line (APP) I know how to find the distance between 2 points using the Distance Formula or Pythagoras I know how to find gradient from 2 points, angle
More informationIntegrated schedule planning with supply-demand interactions for a new generation of aircrafts
Integrated schedule planning with supply-demand interactions for a new generation of aircrafts Bilge Atasoy, Matteo Salani and Michel Bierlaire Abstract We present an integrated schedule planning model
More informationExample of Aircraft Climb and Maneuvering Performance. Dr. Antonio A. Trani Professor
Example of Aircraft Climb and Maneuvering Performance CEE 5614 Analysis of Air Transportation Systems Dr. Antonio A. Trani Professor Example - Aircraft Climb Performance Aircraft maneuvering performance
More informationWind-Based Robust Trajectory Optimization using Meteorological Ensemble Probabilistic Forecasts
Wind-Based Robust Trajectory Optimization using Meteorological Ensemble Probabilistic Forecasts Daniel González Arribas, Manuel Soler, Manuel Sanjurjo Rivo Area of Aerospace Engineering Universidad Carlos
More informationFundamentals of Algebra, Geometry, and Trigonometry. (Self-Study Course)
Fundamentals of Algebra, Geometry, and Trigonometry (Self-Study Course) This training is offered eclusively through the Pennsylvania Department of Transportation, Business Leadership Office, Technical
More informationA Study on Non-Correspondence in Spread between Objective Space and Design Variable Space in Pareto Solutions
A Study on Non-Correspondence in Spread between Objective Space and Design Variable Space in Pareto Solutions Tomohiro Yoshikawa, Toru Yoshida Dept. of Computational Science and Engineering Nagoya University
More informationAVIATION INVESTIGATION REPORT A04A0057 WING SCRAPE DURING A REJECTED LANDING
AVIATION INVESTIGATION REPORT A04A0057 WING SCRAPE DURING A REJECTED LANDING CARGOJET AIRWAYS LIMITED BOEING 727-225 C-GCJB GREATER MONCTON INTERNATIONAL AIRPORT MONCTON, NEW BRUNSWICK 28 MAY 2004 The
More informationFrom structures to heuristics to global solvers
From structures to heuristics to global solvers Timo Berthold Zuse Institute Berlin DFG Research Center MATHEON Mathematics for key technologies OR2013, 04/Sep/13, Rotterdam Outline From structures to
More informationCross-cutting Issues Impacting Operational ATM and Cockpit Usability of Aviation Weather Technology. John McCarthy Sherrie Callon Nick Stoer
Cross-cutting Issues Impacting Operational ATM and Cockpit Usability of Aviation Weather Technology John McCarthy Sherrie Callon Nick Stoer Introduction Air Traffic Management Coordinators are supposed
More informationWeather Impact Modeling. Based on Joe Mitchell s slides
Weather Impact Modeling Based on Joe Mitchell s slides Old Paradigm: Human Centric Weather Aviation traffic manager Forecast Products ATM Automation tailored to aviation needs ready for integration New
More informationWWRP Implementation Plan Reporting AvRDP
WWRP Implementation Plan Reporting AvRDP Please send you report to Paolo Ruti (pruti@wmo.int) and Sarah Jones (sarah.jones@dwd.de). High Impact Weather and its socio economic effects in the context of
More informationVectors are used to represent quantities such as force and velocity which have both. and. The magnitude of a vector corresponds to its.
Fry Texas A&M University Math 150 Chapter 9 Fall 2014 1 Chapter 9 -- Vectors Remember that is the set of real numbers, often represented by the number line, 2 is the notation for the 2-dimensional plane.
More information15-94 Chapter 15: Homework Problems
15-94 Chapter 15: Homework Problems 13.1 Rectilinear Motion (a) The displacement of a particle is given by s = At 3 Bt 2 Ct 50m. If A = 1m/s 3, B = 2m/s 2, and C = 3m/s, plot the displacement, velocity,
More informationInteger Linear Programming Modeling
DM554/DM545 Linear and Lecture 9 Integer Linear Programming Marco Chiarandini Department of Mathematics & Computer Science University of Southern Denmark Outline 1. 2. Assignment Problem Knapsack Problem
More informationAn illustration of the practical use in aviation of operational real-time geostationary satellite data
An illustration of the practical use in aviation of operational real-time geostationary satellite data Jos de Laat # and Jan-Fokke Meirink Royal Netherlands Meteorological Institute operational use of
More information