Research and synthesize remote control loop of flying device using modern control technology

1. Synthetic of remote control law for missile based on application of the optimal control theory of linear systems according to standard quadratic and state observation filter theory;
2. Synthesis of missile stabilizer algorithm based on adaptive control techniques according to reference model.
Synthesis the optimal remote control law based on the model missile parameters at the control station and missile stability adaptive according to the model missile in the onboard stability system is a new solution and reliable highly theoretical and verified, evaluated through simulation, confirming the soundness of the research results.
The proposed algorithms are applicable to synthesize remote control loop and missile stability in current technological and technical conditions, as well as in upgrading, improving and new design of air defense missile complexes.