Optimizationof UAV landing taking into consideration of limitation on control on the basis of solution of the boundary value problem by the parameter continuation

In this article, we investigate the optimal control of flying equipment, taking into account the constraints of UAV landing. When using the Pontryagin maximum principle the optimal control problem is shifted to the boundary problem. To solve the boundary problem, use the parameter continuation method (Parameter continuation method). Control signals are considered as tangential load factors (tangential load factor) and normal load factors (normal load factor). Main research results - The program for optimal control of UAV motion when landing with consideration of limitation of the control signals.