Air-to-air missile direct force/aerodynamic finite time anti-saturation control method
A limited-time, air-to-air missile technology, applied in non-electric variable control, three-dimensional position/course control, vehicle position/route/altitude control, etc., can solve problems such as control force offset, and achieve the effect of closed-loop system stability
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[0062] Specific implementation: Firstly, the longitudinal short-period model of the missile is given, and an integral sliding mode controller that can deal with bounded disturbance and input saturation is designed according to the longitudinal motion model of the missile, and the virtual control torque required to establish the missile overload is obtained. Control distribution is used to map desired control torques to aerodynamic rudder surfaces and direct force devices. Theoretical analysis and numerical simulation both show that the proposed controller can make the compound control missile track overload command signal in finite time, and the closed-loop system is stable.
[0063] In order to avoid the singular phenomenon existing in the traditional terminal sliding mode, a new integral sliding mode surface is proposed, which can make the system state converge to the equilibrium position in a given finite time. According to the longitudinal motion model of the missile, an i...
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