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The problem of maneuvering target tracking is considered in this paper, with an additional (and non-conventional) target attitude measurement, i.e., fusion of data from a point detection sensor with an imaging sensor. This is motivated by the fact that certain attitude variables such as target orientation can provide faster and more reliable information about target maneuvers or acceleration changes...
Bank-to-turn (BIT) missile coordinated autopilot system design principle is presented. The general design concept, design objective and requirement, design approach, and performance analysis are discussed. The closed loop system of the resulting control law is stable for a wide range of flight conditions with little changes in the location of the closed loop eigenvalues. The control loop frequency...
The optimal control theory is applied to the homing missile lateral autopilot design. The approach is to adapt the autopilot gains to the environment model reference and to vary as functions of time-to-go to minimize the performance index. The path constraint is applied throughout the whole terminal homing period and infinite penalty is imposed at intercept. A single-plane, linear autopilot design...
This paper first analyzes and discusses some missile target tracking algorithms. A general formulation of the optimal guidance law using linear state models is then presented for a bank-to-turn missile.
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