无导引头也无惯导导弹的协同制导

doi:10.7527/S1000-6893.2019.23191

Abstract

Abstract: This paper intends to achieve the fire-and-forget attack of the seeker/INS-less missile without relying on the real-time communication and the information of absolute positions of missiles. Two onboard strap-down finders are installed on a seeker-less missile without the Inertial Navigation System (INS) to detect the two specific targets on a seeker-guided missile. Based on these, two cooperative terminal guidance laws are derived for a stationary point target by common negative feedback and finite-time convergence approaches. Another cooperative terminal guidance law is derived for a stationary surface target by the dynamic inverse control. All the aforementioned guidance laws enable the velocity direction of the seeker/INS-less missile point to its attack target before the seeker-guided hits its target. Hereafter, the seeker/INS-less missile can fly straightly to achieve a precise hit. Simulations are conducted to verify the effectiveness and advantages of the proposed guidance laws.

Key words: missile guidance, cooperative guidance, seeker/INS-less missile, fire-and-forget attack, finite-time convergence, surface target

CLC Number:

ZHAO Jianbo, YANG Shuxing, XIONG Fenfen. Cooperative guidance for seeker-less missile without inertial navigation system[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(10): 323191-323191.

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Cooperative guidance for seeker-less missile without inertial navigation system

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