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For the air-breathing hypersonic missile with low overload in cruise phase due to angle of attack restriction, an aerodynamic force and lateral thrust blended control autopilot is designed, which based on fuzzy control theory. The non-linear system model in the longitudinal plane of a hypersonic missile is built, and several fuzzy control strategies are applied in overload command allocation, so as...
A novel guidance law based on extended quadratic cost function is proposed to avoid losing performance index, which is commonly appeared when using cost function with quadratic form. Stochastic optimal guidance laws under target maneuver and target non-maneuver conditions are deducted and are validated by simulating in turn. The simulation results show that guidance trajectories based on extended...
The comparison principle for general continuous time nonlinear Markov jump system is established. Later, using the comparison principle, we obtain some stability criterion, including stability in probability, uniformly stability in probability, asymptotic stability in probability, uniformly asymptotic stability in probability, pth moment stability, pth moment uniformly stability, pth moment asymptotic...
Based on multisensor information fusion theory and optimal control theory of structure stochastic jump system, a new guidance law is proposed for air-to-air missiles based on information fusion of active radar and infrared sensor, and its validity is testified by analysis on simulation by building digital model of missiles. Compared with proportion navigation law and extended proportion navigation...
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