Single Versus Two-Loop Full-State Multi-Input Missile Guidance

摘要

Two types of autopilot-guidance schemes for linear quadratic multi-input missile systems are compared: single-and two-loop configurations. In both cases, all the states are fed back into the guidance loop. In the two-loop case, the inner autopilot loop is designed separately from the outer guidance loop, whereas in the single-loop scheme, the guidance command is injected directly to the actuator, without a definite autopilot It is proven that the two schemes achieve the same performance if and only if the number of guidance commands is identical to the number of available controllers. Thus, using the full-state two-loop scheme may be preferred, because it ensures a stabilized airframe whether the guidance loop is active or not The theorem and guidance laws are illustrated using a dual-control missile model.