The invention discloses a
flexible spacecraft underactuated
system based on the switching control method and an
attitude control method of the
flexible spacecraft underactuated
system based on the switching control method and belongs to the technical field of
spacecraft attitude control. According to the
flexible spacecraft underactuated
system based on the switching control method and the
attitude control method of the flexible
spacecraft underactuated system based on the switching control method, a dynamical model of a flexible
spacecraft with an execution mechanism completely ineffective is established,
coupling, caused by
elastic vibration of a flexible accessory, with a
rigid body is taken as an uncertainty of the system, a dynamical model of a conversion system is a standard
nonlinear model, all states are divided into three sliding model surfaces according to the layering sliding model idea, an
equivalent control component is designed for the first layer of sliding model surface according to the Filippov equivalent theorem, a switching control law is designed by means of the second layer of sliding model surface and the third layer of sliding model surface, and a final control law is formed by combining
equivalent control input and the switching control law. By the adoption of the flexible spacecraft underactuated system based on the switching control method and the attitude control method of the flexible spacecraft underactuated system based on the switching control method, the defect that in the prior art, a flexible spacecraft can not operate normally under the condition that an
actuator becomes ineffective completely during operating of the flexible spacecraft is overcome, and operating reliability of a flexible
spacecraft attitude control system is improved.