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Methods for aircraft guidance with changes in control priorities. (English. Russian original) Zbl 1475.93082

Autom. Remote Control 82, No. 9, 1519-1529 (2021); translation from Avtom. Telemekh. 2021, No. 9, 73-85 (2021).
Summary: We consider various possible implementations of changes in control priorities in aircraft guidance based on time-varying state models, variable penalty coefficients in performance functionals, and allowance for the discrepancy between the interceptor and target dynamic properties. For each possible implementation, specific examples of the guidance method synthesis are given and analyzed.

MSC:

93C95 Application models in control theory
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