Servo Control of a Turbine Gas Metering Valve by Physics-Based Robust Controls (μ) Synthesis

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Servo Control of a Turbine Gas Metering Valve by Physics-Based Robust Controls (μ) Synthesis Dr. Peter M. Young Prof. Electrical Engineering Colorado State University pmy@colostate.edu Dr. Kamran Eftekhari Shahroudi Manager of Analytical Group, Woodward keftek@woodward.com Systems Design and Management Fellow, MIT keftek@sloan.mit.edu

Overview 1. Quick Summary of Robust Controls (μ) Theory 2. Limitations of Current Robust Controls Tools 3. Practitioners Breakthrough: The Physics-Based μ- Synthesis 4. Industrial Application to GS16 Turbine Valves Results Practical Hurdles Experienced Advantages Remaining Problems 5. Recommendations for Future Tool Improvements 6. Sample Woodward Products: Aircraft Engine and Reciprocating Engine Product Portfolio.

1.1 Picture History of Controls by Zhou et. Al. PID s Gain/Phase Margin Simple but fiddly! Ideal when: plant info is scarce. performance not critical. inverse of plant is close to a PID! Robust Design Philosophy Ideal for partially known systems: nominal low order physics is known. uncertainties, variations and disturbances can be bounded. performance is critical over a wide range of conditions. State Space Model/Observer Based Ideal when: MIMO plant info is abundant. performance is critical at specific conditions. Cartoons from the standard text book Robust & Optimal Control by Zhou et. Al.

1.2 Robust Controls: μ- Synthesis & Analysis Basic math framework: Doyle et. Al. ~1988. MATLAB tools ~ 1995. Similar to 6σ philosophy - Design a controller to make the system performance and stability insensitive to bounded operational and behavioral variations by design. - Upfront Robust Design philosophy is at the core of this approach. Find a controller with guaranteed stability and performance margins subject to bounded uncertainties. μ- Analysis is powerful for linear systems: - Can use it to assess robustness no matter how the controller was synthesized. μ- Synthesis has issues because outputs a Magic controller: - Controller states are not physically tractable. - High order controller needs reduction.

1.3 Robust Controller Design Setup Generalized Plant: P - Fuel Metering System - Includes Desired Performance Uncertainties: Δ - Unmodeled Dynamics - Sensor Limitations P Δ Combinations: - Family of Plants Controller: K - MIMO - Sensor Input Vector y - Controller Output Vector u Disturbances: w - Load Disturbances - Friction and Flow Forces - Commands Penalties: z - Tracking Error - Control Energy Objective of μ-synthesis: - Design For Worst Case Signals and Systems -> Robust Performance - Minimize the close loop energy gain from w to z over all frequencies for the whole family of P Δ plants - Locate the easiest way (smallest Δ) to perturb performance and stability.

1.4 Powerful Machinery Under the Hood μ = 1/(size of the smallest destabilizing perturbation) μ Synthesis: Δ P D -1 P D K M K Compute D: μ Problem Compute K: H Problem

2.1 Basic Limitations of Current Robust Controls Tools Basic math theory is sound but the tools output a controller that is physically not tractable or Magic. The Synthesized controllers are high order, complex and not directly practical for many applications. Many (if not most) real plants are non-linear, but the theory and tools are purely linear. Mu Not clear where to add nonlinear compensation Design weights used to drive synthesis are not physically meaningful. Hard to interpret what μ values really mean! 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0-0.1 Robustness analysis mu plots RS NP RP RS-Red NP-Red RP-Red -0.2 10 1 10 2 10 3 10 4 Frequency - rad/s

2.2 Practical Limitations of Current Robust Controls Tools The complete controller design process undefined. μ values do not enable NPI team interdisciplinary collaboration. Visualization of results and trade-offs and comparison with other controllers. How to convince OEM of safety critical machinery to trust this controller. How to debug a problem in the field or during development when the plant states with physical meaning are not available. No features to enable Diagnostics and Prognostics.

3.1 Physics Based μ-synthesis: A practitioner's breakthrough New approach: Physics based μ-synthesis (Builds on available μ-tools in Matlab). Extract reduced order controller or manually design a controller. Use numerical optimization (MATLAB Optimization Toolbox) to match the I/O map of the reduced controller to the full μ-controller. Plot compares the full μ- controller with the final one. Mu 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0-0.1-0.2 Robustness analysis mu plots RS NP RP RS-Red NP-Red RP-Red 10 1 10 2 10 3 10 4 Frequency - rad/s

3.2 Before & After Physics Based μ-synthesis Observer States Before Actual Plant States During Step Observer States After Physically meaningful states help detect problems: e.g. can ask: why is this state not tracking the real plant state?

3.3 The Design Process Requirements Systems Design Optimization Plant Identify System Models Conceptual Design 2 DOF Design Model Physics-Based μ Synthesis Extract Reduced Order Controller Match Reduced Controller to µdesign Continuous to Discrete Test with High Fidelity Model Expensive Very Expensive Preliminary Design Physics-based Controller Convert to Fixed Point Insert H/W Specific Math Test with High Fidelity Model Detail Design H/W Specific Physics-based Controller Generate Embedded Code Test with Real Valve (No Flow) Minimize Expensive Iterations With Robust Controls Complete Valve With Controller Robustness V&V Test with Flow

Resistance UncertaintyIdeal Response Tracking Requirement Sensor Uncertainties 3.4 The 2-DOF Design Model in Simulink Load Disturbance Torque Uncertainty Sensor Noise Controller Nominal Plant

Large nonlinear friction due to stringent turndown ratios and flow accuracy requirements. Stringent Performance and Stability Requirements: positioning accuracy better than 0.005 %. step response 100 ms rise time zero over/undershoot frequency response upper and lower bounds on magnitude and phase response wide operational variations (temperature, pressure, supply voltages, flow loads, friction, command and sensor noise etc). 4. Industrial Application to GS16 Turbine Metering System

4.1 Iteration 1 Results: Measured Robustness to Friction: Step Response Response remained close to ideal (red curve) despite 3 fold rise in friction. Robustness of Step Response to Dry Friction Change from 3 to 9 Amps. Robustness of Step Response to Dry Friction Change from 3 to 9 Amps. Position (Rad) 0.8 0.6 0.4 0.2 STEP0TO90-9A.dyn STEP0TO90-3A.dyn STEP0TO90-6A.dyn Ideal Linear Response Position (Rad) 0.534 0.532 0.53 0.528 0.526 STEP50TO51-9A.dyn STEP50TO51-3A.dyn STEP50TO51-6A.dyn Ideal Linear Response 0 10.1 10.15 10.2 10.25 Time(s) 0.524 0.1 0.15 0.2 0.25 0.3 Time(s) 20 1.5 Velocity (Rad/s) 15 10 5 0 Velocity (Rad/s) 1 0.5 0-5 10.1 10.15 10.2 10.25-0.5 0.1 0.15 0.2 0.25 0.3

4.2 Iteration 1 Results: Measured Robustness to Friction: Frequency Response. Magnitude and Phase response remained ideal up to very high frequencies: despite 3 fold rise in friction! Gain [db] 0-5 -10-15 -20-25 -30 0 SWEEP50TO60-9A.dyn SWEEP50TO60-3A.dyn SWEEP50TO60-6A.dyn SWEEP50TO52-9A.dyn SWEEP50TO52-3A.dyn SWEEP50TO52-6A.dyn Design Target: 2nd Order 40 rad/s, damp=1 Frequency Response Comparison 10 0 10 1 Frequency [Hz] Phase [deg] Coherece x Sig./Noise -100-200 1 0.5 0 10 0 10 1 10 0 10 1 Frequency [Hz]

4.3 V&V : Frequency Response Plot compiles data from 100 tests at extreme conditions. The worst case performance must remain inside bounds. The ability to design to meet specs upfront is key!

4.4 V&V: Step Response Measured step responses at extreme conditions. The worst case rise time must remain below 100 ms (10% to 90% criterion). The ability to design to meet specs upfront is key!

4.5 Practical Hurdles: These problems were not trivial! How to detect coding problems or design mistakes: Incorrect sampling rates. Finding the right balance between gains and sensor limitations. How to cope with design changes: Multi-body dynamics issues as the shaft was extended to add a second position sensor. Numerical overflow problems due to incorrect fixed point scaling. Physics-Based approach always helped because: We could log physically meaningful observer states at run time. We found the source of some problems by checking for physically impossible behavior or checking whether the observer was tracking.

4.6 Experienced Advantages of Physics-Based μ-synthesis Fast Cycle Time or Time to Market benefits since: mistakes are made faster upfront. the iterative work was shifted upfront in the design process. quick resolution of root cause of problems. Re-use benefits (e.g. for next project) since: majority of the work was at a higher abstraction level. Non-linear benefits since: the Physical meaning gave insight and handles to extend the application of a purely linear tool to a highly non-linear problem. V&V Benefits since: minimized the build-test-fix cycle. more robust to spec changes (e.g. bandwidth change). more robust to variation in customer use profile. Easier to explain the function to the rest of the development team.

4.7 Remaining Problems The relationship of design weights and D-scales to physics is not clear. Interpretation of μ-plots in terms of well understood physics are very difficult: Try explaining to NPI team members that we need to reduce friction because μ (the infimum singular value) is too high. Good Luck! Visualization of the μ-analysis results: Which uncertainty, noise, disturbance or plant characteristic is the main robust performance or stability driver at each frequency? How can we trade Robust Performance and Stability?

5. Recommendations for Future Tool Improvements Better visualization and interpretation of μ-synthesis results: Show which elements (e.g. sensor quality, mechanical uncertainties etc.) are driving robust performance and stability at each frequency. The underlying math is there but we need tools to better interpret the results. Link to 6 σ terminology. Develop tools to enable purely physics driven μ-synthesis process: Physics of Design Weights and States Meaning of D-Scales. Useful decomposition. Approximately retaining physical meaning after reduction. For more information please read: Paper by K E Shahroudi in IEEE TCST 2006, vol. 14, no6, pp. 1097-1104. Presentation by the same authors at ACC 2007 Conference in New York this summer.

Conclusions We have measured unprecedented robust performance and stability in a very tough industrial controls application. We built a Physics-Based Robust Controller Synthesis Process on top of existing Matlab Toolboxes (μ-tools, Optimization and Simulink). Robust Design Philosophy is infusing many large OEM s (such as GE) but the difficulty is: How to generate robust designs upfront by synthesis rather than buildtest-fix cycles. How to relate their normal robustness measures to metrics they already understand (e.g. Six Sigma terminology). We believe these approaches can shine for highly complex MIMO type problems elsewhere. We identified some key directions for improving the Robust Controls Synthesis tools.

6.1 Integrated Energy Control and Optimization Solutions from Woodward: Aircraft Engine Systems Integration Fuel Systems Fuel Metering, Pump, Actuation, Air Valves, Specialty Valves. Combustion System Fuel Injection, Ignition, Manifolds, Sensors. Heat Management Heat Exchangers, Lube and Scavenge Pumps, Filtration System, Fuel/Oil Sensors. Electrical System Electronic Control, Sensor Suite and Power Systems. See www.woodward.com for details

6.2 Integrated Energy Control and Optimization Solutions from Woodward: Reciprocating Engine See www.woodward.com for details