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Based on stochastic maximum principle, the optimal control algorithm is proposed for Markov jump system with Constrained Control Input. With statistical linearization method, the parametes of the optimal controler can be achieved by solving a Riccati function. Finally the simulation examples are given to test and verify the function of optimal controller designed in this paper.
An algorithmic method to calculate angle precision of remote target by dual-aircraft cooperatively passive location is performed. Firstly, with some proper hypotheses, an analytic model of dual-aircraft cooperatively locating remote target based on Direction of Arrival (DOA)is set up. Then the mathematic relationship between azimuth angle and Time Difference of Arrival (TDOA) based on wave path difference...
A new guidance law is proposed for Near Space Hypersonic Vehicle (NSHV) based on multiple model theory and optimal control theory of structure stochastic jump system. By choosing different character velocities of the NSHV in near space and aero space, different motion models for the NSHV of three-DOF are constructed. Then, for each model, a guidance law is developed by the proposed method. These guidance...
The longitudinal motion model of a winged-cone configuration near space hypersonic flight vehicle is presented. Then the constituted nonlinear motion equations are linearized under different flight height and velocity to form a series of linear systems by small disturbance method. Each linear model is considered as a mode of a Markov jump system, which in whole make up a Markov jump system for the...
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