Suboptimal attitude control system for Nimbus satellite using motor-driven inertia wheels as control torque source for three dimensional control
On the synthesis of suboptimal, inertia-wheel attitude control systems.
GUIDANCE AND CONTROL IN SPACE, INTERNATIONAL FEDERATION OF AUTOMATIC CONTROL, CONGRESS ; 1969 ; WARSAW, POLAND
1969-01-01
Conference paper
No indication
English
Design considerations of inertia wheel systems for attitude control of satellite vehicles
Engineering Index Backfile | 1962
|Inertia-free Spacecraft Attitude Tracking with Reaction-Wheel Actuation
British Library Conference Proceedings | 2010
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