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Active Defense Line-of-Sight Guidance Law with Compensation of Unknown Disturbance for the Cooperation of Aircraft and Interceptor
Jie WANG, Junhui LIU, Hao CHEN, Qi ZHAO, Wei LIU
Modern Defense Technology    2024, 52 (2): 94-103.   DOI: 10.3969/j.issn.1009-086x.2024.02.011
Abstract133)   HTML3)    PDF (1390KB)(238)       Save

With the development of unmanned military technology, unmanned short-range air combat has attracted much attention from military powers in the world. Faced with the threat of high-speed and high-maneuverability attacker missiles, traditional passive defense measures such as throwing chaffs or releasing hot flame bombs fail to ensure the safe escape of target aircraft. It is a feasible method to implement active defense by launching defender missiles to coordinate the maneuvering of target aircraft. However, due to the strong maneuverability of the attacker missile and unknown acceleration information, it is difficult to design the guidance law of cooperative target aircraft-missile. An active defense line-of-sight (LOS) guidance law based on disturbance compensation was proposed in this paper. A nonlinear disturbance observer was designed to estimate the influence of the maneuverability from the attacker missile, which was compensated for in the design of active defense LOS guidance law for the cooperation of aircraft and missile. The results of the simulation indicate that the method used in this paper can effectively defend the attacker missile with unknown maneuverability. The study in this paper thus provides a reference for the three-body attack and defense problem.

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Optimal Deployment of Defense Weapons under Point Defense
LIU Yao, ZHANG Zhan-yue, HUANG Zi-chen, ZHAO Cheng-liang
Modern Defense Technology    2018, 46 (5): 52-61.   DOI: 10.3969/j.issn.1009-086x.2018.05.09
Abstract299)            Save
In view of the strategic defense problem, according to different operations two scenes including a single-directional threat and a fan-shaped threat are established, and the incoming targets are intercepted at the middle segment. According to the characteristics of the selected interceptor and the incoming missile, the space killing area of the interceptor mode and the model of protection zone and the covering angle of the ground assets are established, and the weapon deployment model under the two scene defense systems is established. The model is optimized by the comprehensive interception efficiency, the ground assets covering angle, and the deployment cost. The validity of the deployment model method is verified by a concrete example. The research results have certain reference value for the application of antimissile warfare.
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