A Design Method for an Optimal Attitude Regulator for a Spinning Space Station
1967
41 pages
Report
No indication
English
Astronautics , Attitude control , Feedback control system , Linear system , Optimal control , Space station , Attitude , Control , Digital , Feedback , Gain , Linear , Optimal , Regulator , Simulation , Space , Station , System , Time
Attitude control of flexible, spinning, toroidal manned space station
Engineering Index Backfile | 1967
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