Specific features of the attitude stabilization system synthesis for high precision unmanned aerial vehicles

The main features of attitude stabilization system are considered that are necessary to take into account when designing the full automatic vehicle control system. The details of adaptation algorithms realization are defined that are ignored in the adaptive system analytic synthesis. The problem is solved of providing the control signals constraints at their kinematic decoupling for the vehicles with three control surfaces. The analytical algorithm is given of angle of attack evaluating during the flight.