To solve the problem of multiply missiles with varying velocities attacking the target simultaneously, a cooperative guidance strategy with impact time and angle constraint is proposed. Firstly, a three-dimensional cooperative guidance model is presented by establishing the kinematics and dynamics equations of each missile, the relative motion relationship between the missile and the target is derived. Then a time-to-go method with time-varying velocities is designed. Considering the constraint of field of view angle and attack angle, the three-dimensional cooperative guidance law is designed based on offset proportional guidance method. Finally, simulation results verify the effectiveness and superiority of the proposed guidance law.
Three-Dimensional Cooperative Guidance Law with Time-Varying Velocities
Lect. Notes Electrical Eng.
International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022
2023-01-31
9 pages
Article/Chapter (Book)
Electronic Resource
English
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