electromechanical actuation for launch vehicles · electromechanical actuation for launch vechicles...
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ELECTROMECHANICAL ACTUATION FOR
LAUNCH VECHICLES
Presented By:Mark A. Davis
Moog Inc.
37th AIAA/ASME/SAE/ASEEJoint Propulsion Conference
Salt Lake City, UtahJuly 10, 2001
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MOOG
Introduction
This paper describes recent developments in Electromechanical Actuation applied to Launch Vehicles. The following topics are discussed:
4 Electromechanical (EM) Actuation System Design
4 Comparison of Electromechanical and Electrohydraulic Actuation Systems
4 High Power EM Thrust Vector Control (TVC) Systems
4 Redundant EM TVC Systems
4 Propellant Valve Electromechanical Actuation
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Electromechanical TVC Actuation System
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MOOG
Electromechanical Servoactuator System
Permanent Magnet Brushless MotorSinusoidal Motor Drive
A+ B+ C+
A- B- C-
A+A-B+B-C+C-
MODULATORWIDTHPULSE
CONTROLLERCURRENT
COMMUTATIONELECTRONIC
CONTROLLERSERVO
CONVERTERSIGNALRESOLVER
DEMODULATOR
RESOLVER
REDUCTIONGEAR
SCREWBALL
EXCITERAC LVDT
POSITIONOUTPUT
MOTORBRUSHLESS
MOTOR PHASE CURRENT
MOTOR POSITION
ACTUATOR POSITION
MOTOR VELOCITY
COMMANDPOSITION
BATTERY VOLTAGE
L5112.DRW
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MOOG
Comparison of EM and EH Actuation Systems
Advantages of Conventional Electrohydraulic Systems
4Mature Technology
4 High Reliability
4 Can Use Relief Valves to Limit Piston Force• Effective to Handle Impulse Load
4 Continuous Stall Torque Capability
4 High Acceleration Capability
4 No EMI Generation
4 Simple, Low Power Electronics
4Mature Redundancy Implementation
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MOOG
Comparison of EM and EH Actuation Systems
Advantages of Electromechanical Systems4 Excellent Long-Term Storability4 Easy Checkout4 Easy Installation4 Low Maintenance4Minimal Operations Cost4 Low Quiescent Power4 No Fluid Leakage4 No Concern for Fluid Contamination4 High Reliability4 Lower Weight than Hydraulic Blowdown TVC Systems
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Limitation of EM Actuation Systems
Typical EM System Frequency Response Limits
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MOOG
38 HP EM TVC ACTUATOR Dual Torque-Summed Motors
Output Travel…….+/- 5.5 in Impulse Load ….. 100,000 lb Stall Force …………55,000 lb Acceleration……..60 in/sec^2Rated Power………..38 HP Duty Cycle………10 min
Output Force……..48,000 lb Average Load…15,000 lbOutput Velocity…..5.2 in/sec Supply Voltage….270 VDC
Full Performance with one motor
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MOOG
38 HP EM Actuation System
Force-Velocity Test Data On SSME Test Fixture
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MOOG
38 HP EM Actuation System
Frequency Response Test Data On SSME SimulatorLoad Position Response (+/- 2 % COMMAND)
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MOOG
38 HP EM Actuation System
Frequency Response Test Data On SSME SimulatorLoad Position Response (+/- 5 % Command)
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Controller
Controller Critical to Performance of EM Systems
Breadboard Controller Used to Demonstrate 38 HP EM TVC System
Development of Flight Worthy High Power EM Controller
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MOOG
Moog DSP-Based Digital Controller
Digital Loop ClosureIGBT Power Stage320 VDC Maximum Supply Voltage200 Amps Peak Motor Phase CurrentVector Control / Sinusoidal Motor DriveDemonstrated with a 20 HP EM TVC Actuator
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EM TVC Actuators For Large Solid Rocket Motors
Two TVC Actuators Have Been Demonstrated
12 HP 21 HP --- Brushless PM MotorStall Force (lb) 4600 31,000 --- BallscrewStroke (in) +/- 1.92 +/- 1.5 --- LVDT Length (in) 15.5 17.0Power Point
Velocity (in/sec) 20 5.85Force (lb) 4000 24,000
Weight (lb) 16 75Voltage (VDC) 280 280
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MOOG
Upper Stage Redundant EM TVC Systems
Flight ProvenActive-Standby RedundancyFull Performance with one motor operatingSix-Step Motor Drive
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MOOG
Upper Stage Redundant EM TVC Systems
Typical Performance Summary
Stroke +/- 0.75 inStall Force 2000 lbNo-load Velocity 3.0 in/secOutput Power 0.4 HP Frequency Response 90 deg phase @ 4.3 HzActuator Length 23.25 inSupply Voltage 28 VDCElectrical Interface MIL-STD-1553Actuator Weight 17 lb eachController Weight 27 lb
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MOOG
Upper Stage TVC System Block Diagram
Active-Standby RedundancyFull Performance With One Motor Operating
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MOOG
Propellant Valve EM Actuation Systems
Dual Redundant Brushless MotorsHarmonic Drive Provides Rotary OutputRedundant Controller
Typical PerformanceStroke……………...+/- 70 degOutput Power………..0.05 HP
Velocity………..340 deg/secTorque…………..60 in-lb
Actuator Weight…….8.2 lbController Weight….21.3 lbVoltage …………….28 VDC
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MOOG
Summary
Electromechanical Actuation is a Reality for Launch Vehicles
4
Flight Proven EM TVC Systems on Upper Stages
High Power Applications (Booster TVC Systems)
4
EM Actuation is a Viable Alternative to Electrohydraulic Actuation
4
High Power EM TVC Systems are Flight Ready
4
EM TVC Systems Offer the Potential of:• Lower Life Cycle Cost• Lower Weight