3 edition of Distributed control using linear momentum exchange devices found in the catalog.
Distributed control using linear momentum exchange devices
by National Aeronautics and Space Administration, George C. Marshall Space Flight Center, For sale by the National Technical Information Service in [Marshall Space Flight Center, Ala.], [Springfield, Va
Written in English
|Statement||By John P. Sharkey, Henry Waites, and George B. Doane III.|
|Series||NASA TM -- 100308., NASA technical memorandum -- 100308.|
|Contributions||Waites, H. B., Doane, George B., George C. Marshall Space Flight Center.|
|The Physical Object|
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Get this from a library. Distributed control using linear momentum exchange devices. [John Patrick Sharkey; Henry Waites; George B Doane; George C. Marshall Space Flight Center.]. Page - Asymptotic Stability Theorem for Autonomous Systems," Journal of Guidance, Control, and Dynamics, Vol.
16,pp. Appears in. momentum, and internal torques exchange momentum between different rotating parts of the spacecraft. In this way reaction wheels or control moment gyroscopes may be used to change spacecraft pointing without affecting total angular momentum.
Because environmental disturbances create external torques on the spacecraft, they also create angular. Considerations in Using Momentum Exchange Devices and Reaction Jet Thrusters for Active Control Tutorial Summary Bibliography 26 Tutorial on Other Flight Vehicles Tutorial on Helicopter (Rotorcraft) Flight Control Systems.
book. Analytical Mechanics Linear Coupled Attitude-Orbit Control Through Aerodynamic Drag. Journal of Guidance, Control, and Dynamics Studies the dynamic modeling and control of spacecraft containing multiple momentum exchange devices, and/or flexible spacecraft components.
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A new initial Distributed control using linear momentum exchange devices book and attitude-acquisition control-law using skewed wheels. Unique attitude maneuver-strategy and pointing control schemes for the bias momentum system with four skewed wheel configuration.
A large angle maneuver strategy for the biased multi-wheel system. Filipe. N, and Tsiotras, P., "Simultaneous Position and Attitude Control Without Linear and Angular Velocity Feedback Using Dual Quaternions,'' American Control Conference, Washington, DC, June 17.
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Space Vehicle Dynamics and Control, Second Edition continues to provide a solid foundation in dynamic modeling, analysis, and control of space vehicles featuring detailed sections covering the fundamentals of controlling orbital, attitude, and structural motions of space vehicles.
A new Part 5 is a collection of advanced spacecraft control problems and their practical. Li, Z. and Bainum, P. M., “ Vibration control of flexible spacecraft integrating a momentum exchange controller and a distributed piezoelectric actuator,” J.
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Visit Stack Exchange. Nonlinear Spacecraft Stability and Control Introduction Nonlinear Stability Analysis Generating Lyapunov Functions Nonlinear Feedback Control Laws Lyapunov Optimal Control Laws Linear Closed-Loop Dynamics Reaction Wheel Control Devices Variable Speed Control Moment Gyroscopes References Problems Part 2.
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