Exponential Time-varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver of Rigid Spacecraft
نویسندگان
چکیده
منابع مشابه
Time-varying Exponential Stabilization of the Attitude of a Rigid Spacecraft with Two Controls Time-varying Exponential Stabilization of the Attitude of a Rigid Spacecraft with Two Controls
Rigid body models with two controls cannot be locally asymptotically stabilized by continuous feedbacks which are functions of the state only. However, this impossibility does no longer hold when the feedback is also a function of time, and explicit smooth time-varying feedbacks which locally asymptotically stabilize the attitude of a rigid spacecraft have previously been proposed by the author...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2010
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(09)60240-5