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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...
This paper summarizes a combined midcourse and terminal guidance and control law design of missiles to achieve range enhancement and stability with excellent intercept performance. We derive analytic solutions of a closed loop, nonlinear optimal guidance law for three dimensional flight for both the midcourse and terminal phases. Since this combined guidance law contains the proportional navigation...
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