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. In this paper a new thruster pulse-modulation scheme for pointing and tracking applications is developed from nonlinear control theory.
A Robust Digital Autopilot for Spacecraft Equipped with Pulse-Operated Thrusters
1996-01-01
Preprint
Keine Angabe
Englisch
Robust Digital Autopilot Design for Spacecraft Equipped with Pulse-Operated Thrusters
Online Contents | 1996
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