发明授权
US08209065B2 Steering logic for spacecraft slew maneuvers 有权
航天器转向动作的转向逻辑

Steering logic for spacecraft slew maneuvers
摘要:
Spacecraft control modules can steer a spacecraft during a slew maneuver. The spacecraft control modules can receive a target attitude for the spacecraft slew maneuver. An angle between a current attitude and the target attitude may be determined. A smooth attitude offset profile with respect to a steering frame may be established from the current attitude to the target attitude. A smooth attitude command may be generated from the smooth attitude offset profile. The smooth attitude command may be applied to an attitude control module of the spacecraft.
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