V.I. Merkulov, I.V. Zabelin, A.M. Kuimov, D.A. Milyakov
A study of an algorithm of trajectory control of airborne radar carrier which provides resolution of airborne objects in a dense cluster was conducted in order to ascertain the algorithm’s restrictions.
Influence of required linear resolution, radar bandwidth, penalties for guidance accuracy for angular rate and control signal magnitude on trajectory and phase coordinates was considered. The studied algorithms was proved to allow resolution of objects in a dense cluster on initial guidance stage and to provide guidance on a selected target on the final stage of guidance without restrictions on its implementation.