Exploring New Lagrangian Cyclers to Enhance Science: Communications with CubeSat Technology
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1 Publications Exploring New Lagrangian Cyclers to Enhance Science: Communications with CubeSat Technology Pedro P. Llanos Embry-Riddle Aeronautical University, Abdiel Santos Galindo Embry-Riddle Aeronautical University John Ford Embry-Riddle Aeronautical University Follow this and additional works at: Part of the Space Vehicles Commons Scholarly Commons Citation Llanos, P. P., Santos Galindo, A., & Ford, J. (2015). Exploring New Lagrangian Cyclers to Enhance Science: Communications with CubeSat Technology., (). Retrieved from This Presentation without Video is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Publications by an authorized administrator of Scholarly Commons. For more information, please contact
2 Exploring New Lagrangian Cyclers to Enhance Science: Communications with CubeSat Technology Pedro J. Llanos, Ph.D. Abdiel Santos Galindo John Ford ISS R&D Conference July 6 th - 9 th, 2015 Embry-Riddle Aeronautical University Daytona Beach, FL 1
3 Outline Introduction CubeSat Technology Mathematical Model Results (Matlab and STK) CubeSat Performance Future Work: Applications References Photo Credit: NASA 2
4 Introduction Novel Cyclers Trajectories for CubeSats that will depart from Low-Earth Orbit and provide significant opportunities to enhance communications and navigation strategies while advancing exploration capabilities Photo Credit: NASA 3
5 CubeSat Technology Developed by Cal Poly and Stanford University Unit: 1U (10cm x 10cm x 10cm) Small Spacecraft Accessible for Public, Industry and Government High Asset for Spacecraft Flight Opportunities and mission development Low Cost Photo Credit: NASA 4
6 Mathematical Model. L 4 EARTH MOON... L 3 L 1 L 2 Photo Credit: NASA / LPI-JSC. L 5 5
7 Mathematical Model Motion of infinitesimal mass in the rotation frame can be described by the governing equation of motion: Circular Restricted Three-Body Problem (CRTBP) Earth, Moon and CubeSat Rotating frame 6
8 Results (Matlab and STK) ISS to Earth-Moon L1 (Scenario 1) CubeSat departs ISS and does an Orbital Transfer to EML1. Earth-Moon L2 to Earth-Moon L1 (Scenario 2) CubeSat shows capability to transfer between Libration Points. Photo Credit: NASA Minor stationkeeping maneuvers for both scenarios with low V 7
9 Scenario 1 : From ISS to Earth-Moon Lagrange Point L1 (EML1) 1: ISS Departure 2: Earth Departure 3: Earth Transfer to EML1 4: Arrival at EML1 8
10 Results (Matlab and STK) Scenario 2 : CubeSat from Earth-Moon L2 to Earth-Moon L1 1: Arrival from Earth 4: Two-Revolutions around EML1 3: One Loop around the Moon 2: Six-Revolutions at EML2 9
11 Scenario 1 (ISS to EML1) Results: STK Simulations Exploring New Lagrangian Cyclers to Enhance Science: Communication with Cubesat Technology 10 10
12 Results (Matlab and STK) Scenario 1 (ISS to EML1) ISS departure ΔV = km/s Time of flight = 4 days 9 hours EML1 (Orbit Insertion + SK) ΔV = 740 m/s Number of Orbits = 2 Time in Orbit = 17 days and 7 hours Scenario 2 (EML2 to EML1) EML2 (Orbit Insertion + SK) ΔV = km/s Number of Orbits = 6 Time in Orbit = 2 months and 11 days EML2 to EML1 transfer ΔV = 350 m/s Time of Transfer = 17 days SK=Stationkeeping EML1 (Orbit Insertion + SK) ΔV = 370 m/s Number of Orbits = 2 Time in Orbit = 24 days 11
13 Results: Novel Cyclers QSO between EML1 and EML2 QSO in Earth s vicinity QSO Paraboloid Moon Moon 12
14 Results: Novel Cyclers QSO going through gate EML1 connecting Earth & Moon 5:3 QSO in EM system EM L4/L5 Asymmetric Orbits 13
15 CubeSat Performance PowerCube up to 6m/s per orbit (Electrolysis) Pictures and Data courtesy of: Tethers Unlimited HYDROS Thruster - scalable to >2km/s (Electrolysis) MicroPET raising propellantless system (Electrodynamic Tethers) 14
16 Future Work: Applications Science and Communication Gravitational Field Mapping Cislunar or Interplanetary CubeSat Space Weather Monitoring Low Data Rate communications with fleet of CubeSat Technology testing for Mars and its Moons (AIAA ) Photo Credit: NASA (INSPIRE) CubeSat project 15
17 Future Work: Applications Orbital Debris Monitoring ISS Departure (400km) to Low Earth Orbit (725km) Debris Resistive/Acoustic Grid Orbital Navy Sensor (DRAGONS) Better understanding of MicroMeteroid and Orbital Debris (MMOD) Impact avoidance for ISS and reduction of collision avoidance maneuvers. Orbit Maintenance CubeSat deployment from ISS (NanoRacks); JEM (Cyclops launcher), Orbital (Jupiter/Exoliner) and Suborbital flight vehicle (example: Lynx Mark III) deploying the CubeSat from its dorsal pod using a dual stage rocket. Satellite Stationkeeping, safe deorbit, repair, maintenance. Picture credit: Lynx 16
18 References [1] P. J. Llanos, G. R. Hintz, M. W. Lo, and J. K. Miller, Heteroclinic, Homoclinic Connections between the Sun-Earth Triangular Points and Quasi-Satellite Orbits for Solar Observations, Vol. AAS/AIAA, Astrodynamics Mechanics Meeting, AAS , [2] M. W. Lo, The interplanetary superhighway and the Origins Program, Vol. IEEE Aerospace Conference, Big Sky, MT, USA, [3] J. E. Marsden and S. D. Ross, New Methods in Celestial Mechanics and Mission Design, Vol. 43,1, 2006, pp [4] S. Ross, The Interplanetary Transport Network, Vol. Sigma Xi, The Scientific Research Society, [5] K. Harris, M. McGarvey, H. Y. Chang, M. Ryle, T. R. II, B. Udrea, and M. Nayak, Application for RSO Automated Proximity Analysis and IMAging (ARAPAIMA): Development of a Nanosat-based Space Situational Awareness Mission, Vol. 27th Annual AIAA/USU Conference on Small Satellites, SSC13-WK-6, [6] I. Tether Unlimited, Transformative Technologies for Space, Sea, Earth, and Air, Vol. accessed on July 1, [7] P. J. Llanos, Trajectory Mission Design and Navigation for a SpaceWeather Forecast, Vol. Ph.D Thesis, University of Southern California, [8] N. O. D. P. Office, Orbital Debris Quaterly News, Vol. 16, Issue 3, National Aeronautics and Space Administration, July [9] H. Helvajian and S. W. Janson, Small Satellites: Past, Present and Future, AIAA, Inc., The Aerospace Corporation,
19 Thank you for your attention Questions? Photo Credit: ESA 18 View publication stats
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