Actuator Force Using Physical Modeling Tools to Design Power Optimized Aircraft

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Actuator Force Using Physical Modeling Tools to Design Power Optimized Aircraft 2009 The MathWorks, Inc.

Key Points 1. Testing different actuator designs in one environment saves time and encourages innovation 2. Optimizing systems with respect to design requirements leads to optimal design choices Aileron Angle Actuator Force 3. Simulating at different levels of fidelity is required to see effects of design implementation 2

Agenda Trends in the aerospace industry 10 min Industry trends Strategies for improvement How simulation can help Example: Flight Actuation System 15 min Model explanation Tradeoff study System optimization Assess implementation effects Conclusions 3

Industry Trends System needs Aircraft must produce less pollution Aircraft must be more efficient Example goals Clean Sky (for year 2020) 50% reduction of CO 2 emissions 80% reduction of nitrous oxide emissions Power Optimized Aircraft (POA) 25% cut in peak non-propulsive power 5% reduction in fuel consumption With 5-6 C warming existing models estimate an average 5-10% loss in global GDP. Head of the Government Economic Service UK, 2006 Research project, EU and industry Strategies include aircraft-level optimization, technology 4

Strategies for Improved Aircraft Design Technology: Electrical actuation Fewer losses than hydraulic actuation Only needs to be turned on when in use Tend to be more reliable, cleaner, and safer Aircraft-level optimization Consolidation of power electronics Localize hydraulic actuation Boeing 787 Electrical Systems Brakes Ice protection Engine start Environmental controls Electrohydraulic pumps Airbus 380 Electrical Systems Primary flight control actuators Thrust reverser actuation Horizontal stabilizer backup Simulation can help with each of these strategies 5

How Simulation Can Help 1. Tradeoff studies to test electrical and hydraulic systems Determine actuator requirements Test hydraulic and electrical actuator designs 2. System-level models Must be done at aircraft level to optimize architecture Few key parameters and quick simulation 3. Simulating at different levels of fidelity Need to easily add fidelity to see impacts of implementation Reuse work done at system level (Model-Based Design) 6

Example: Aileron Actuation System System Actuation Simulation goals 1. Determine requirements for actuation system 2. Test performance with electrical or hydraulic actuation 3. Optimize the actuation system 4. Assess effects of system implementation 7

Determing Actuation Requirements Model: θ Aileron Ideal Actuator Problem: Determine the requirements for an aircraft aileron actuator Solution: Use SimMechanics to model the aileron and Simscape to model an ideal actuator 8

Test Electrical and Hydraulic Designs Model: Hydraulic Actuator Electromechanical Problem: Test different actuator designs in the system Solution: Use SimHydraulics and SimElectronics to model the actuators, and configurable subsystems to exchange them 9

Actuator System-Level Designs Hydrostatic transmission Electromechanical system Speed Current Variable-displacement pump Double-acting hydraulic cylinder Replenishing valves Pressure-relief valves Charge pump Speed controller DC Motor Worm gear Current sensor and current controller Hall effect sensor and speed controller PWM and H-bridge driver 10

Optimize System Performance Model: Angle Current ω Speed i Current Problem: Optimize the speed controller to meet system requirements Solution: Use Simulink Design Optimization to tune the controller parameters ω Speed K p K i 23.4 0.3 3.67 0.3 11

Assess Implementation Effects Model: Current ω Speed i Current 1 s Simulink Circuit Averaged PWM Problem: Assess the effects of design implementation on system performance Solution: Use SimElectronics to add a PWM signal and analog circuit implementation ω i 12

Conclusion 1. Testing different actuator designs in one environment saves time and encourages innovation 2. Optimizing systems with respect to design requirements leads to optimal design choices Aileron Angle Actuator Force 3. Simulating at different levels of fidelity is required to see effects of design implementation 13

Multidomain physical systems SimElectronics SimDriveline SimHydraulics Simscape SimMechanics SimPowerSystems MathWorks Products Used Simscape MATLAB, Simulink SimMechanics SimHydraulics Hydraulic (fluid power) systems SimElectronics (new) 3-D mechanical systems Electronic and electromechanical systems Simulink Design Optimization Actuators & Sensors Drivers Semiconductors 14