Abstract:

To avoid the shortcomings in the choice of decision variable, heuristic function and route expression, this paper proposes a new heuristic route planning approach that features some key threat points. The angle of attack, sideslip and roll are used as independent decision variables for decision-making. The cost function takes several factors into consideration, such as threat degree, overload and the distance to destination. Dynamic and kinematic constraint equations of the missile are established and a smooth trajectory is generated by Runge Kutta (R-K) integral. Finally, taking the bacd to turn (BTT) lateral symmetric long range supersonic missile as an example, simulation experiments are carried out to demonstrate the feasibility of the approach, which satisfies various constraints and can obtain an optimal route rapidly.