Robust digital autopilot design for spacecraft equipped with pulse-operated thrusters

The analysis and design of attitude control systems for spacecraft employing pulse-operated (on-off) thrusters is usually accomplished through a combination of modeling approximations and empirical techniques. A new thruster pulse-modulation theory for pointing and tracking applications is developed...

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Bibliographische Detailangaben
Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 1996-09, Vol.19 (5), p.1047-1055
Hauptverfasser:	Thurman, Sam W, Flashner, Henryk
Format:	Artikel
Sprache:	eng
Schlagworte:	Approximation Automatic pilots Computer simulation Control theory Design specifications Digital computers Errors Lyapunov methods Mathematical models Nonlinear control systems Pulse modulation Robustness (control systems) Thrusters Time varying systems Torque Vehicles
Online-Zugang:	Volltext
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