Active center of gravity (C.G.) control is a key technology of vehicle management system, which has been extensively used in various types of aircraft. With active C.G. control system, aircraft may deviate from its known dynamics due to the C.G. offset, thus bringing new problems to the existing flight control system. A new design approach of the attitude control system of aircraft with C.G. variations is proposed in this paper.
Modeling and attitude control of aircraft with center of gravity variations
01.03.2009
342374 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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