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The integrated guidance and control (IGC) technology of aircraft has been developing for more than 30 years, and it mainly focused on the research in single plane. Due to the exigent requirement on the three-dimensional IGC technology in current researches, the mathematical modeling in three-dimensional space is considered and analyzed in order to solve the primary problem during the design period...
Aiming at attitude control of spacecraft, the method of fuzzy reaching law sliding mode is introduced. Firstly, the spacecraft dynamics equation based on angular velocity and kinematic equation based on error quaternion are introduced. Then according to the mathematical model of the satellite attitude control system, the sliding mode controller is designed while the stability of the system is proven...
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