Full-State Autopilot-Guidance Design under a Linear Quadratic Differential Game Formulation
نویسندگان
چکیده
Full-state single-loop and full-state two-loop autopilot-guidance designs are derived using a linear quadratic differential game formulation. To keep all the states at reasonable values throughout the end-game, a cost function that includes appropriate running cost terms on some of the states is proposed. It is proven that the two designs may be identical under a linear quadratic differential game formulation and the proposed cost function. The theorem and guidance laws are illustrated using an interceptor missile having forward and aft controls.
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