Attitude control/momentum management of the Space Station Freedom for large angle torque-equilibrium-attitude configurations

1990 ◽  
Author(s):  
ALEXANDER PARLOS ◽  
JOHN SUNKEL
Keyword(s):  
Attitude Control ◽  
Large Angle ◽  
Space Station ◽  
Space Station Freedom ◽  
Momentum Management

Robust Output Regulation Approach for Attitude Control and Momentum Management of the Space Station

2015 ◽  
Vol 719-720 ◽  
pp. 316-323
Author(s):  
Yong Liu ◽  
Wei Huo
Keyword(s):  
Attitude Control ◽  
Closed Loop ◽  
Space Station ◽  
Output Regulation ◽  
Management Problem ◽  
Closed Loop System ◽  
Model Uncertainties ◽  
Robust Output Regulation ◽  
Regulation Approach ◽  
Momentum Management

An novel methodology to solve the attitude control and momentum management problem of the space station with model uncertainties is developed. By the use of the robust output regulation theory, the attitude control and momentum management integrating model and the internal model of disturbances are combined to design a robust coupling controller such that the plant outputs track desired reference signals and the model uncertainties can be tolerated. It is proved that the designed controller guarantees stability of the closed-loop system and suppresses the disturbance well. Simulation results are provided to demonstrate the feasibility of the proposed method.

Robust Approach to Attitude Control and Momentum Management for Space Station

2014 ◽  
Vol 644-650 ◽  
pp. 578-585
Author(s):  
Bing Han ◽  
Wei Huo
Keyword(s):  
Attitude Control ◽  
Closed Loop ◽  
Space Station ◽  
Optimal Controller ◽  
Parameter Uncertainties ◽  
Robust Approach ◽  
Loop Region ◽  
Simulation Results ◽  
Rank Decomposition ◽  
Momentum Management

A novel methodology to design a robust attitude control and momentum management controller for the space station is proposed. Firstly, the method of maximum rank decomposition is adopted to deal with parameter uncertainties independently. Secondly, based on the resulted model, an optimal controller, with closed-loop region pole constraints, is designed. Finally, simulation results are presented to demonstrate the control effects.

Momentum management and attitude control design for a Space Station

1988 ◽  
Vol 11 (1) ◽  
pp. 19-25 ◽  
Author(s):  
Henry H. Woo ◽  
Henley D. Morgan ◽  
Eric T. Falangas
Keyword(s):  
Attitude Control ◽  
Space Station ◽  
Control Design ◽  
Momentum Management
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