An approach to digital control system design is applied to the analysis and design of a practical onboard digital attitude control system for a class of spinning vehicles characterized by a rigid body and two connected flexible appendages. The approach used is to design a continuous-data control system that will provide a satisfactory system response. Then, using the digital redesign method, a digital controller with onboard digital computer is designed to provide a digital control system whose states are similar to those of the continuous system at sampling instants. The simplicity of application of this approach is indicated by example. The example, using spinning Skylab parameters, is used to substantiate the conclusions.
Design of a digital controller for spinning flexible spacecraft
AIAA Guidance and Control Conf. ; 1973 ; Key Biscayne, FL, United States
1974-04-01
Report
Keine Angabe
Englisch
Digital Control of Spinning Flexible Spacecraft
AIAA | 1978
|Digital control of spinning flexible spacecraft
AIAA | 1977
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