Design of thrust regulation law for adjustable lateral thrust and aerodynamics blended control aerocraft

摘要

The thrust regulation law for adjustable lateral thrust and aerodynamics blended control aerocraft is proposed in this paper. Firstly, lateral jet engine configuration and thrust characteristics are given, while the constraint conditions are analyzed. Secondly, the dynamic model of thrust regulating process is established, and the cost function and constraint conditions of the optimization problem are determined. In addition, the thrust regulation law is proposed based on dynamic system method. Then, the analytical form of the regulation law is presented by analyzing thrust regulation process of different quadrants. Finally, the feasibility of the thrust regulation law is verified by the simulation results.