Adaptive internal model guidance law for weaving maneuvering target. (September 2017)

• Record Type: Journal Article
• Authors: Deng, Xiangfei; Liu, Xiangbin
• Is Part Of: ISA transactions. Volume 70(2017:Sep.)
• Page Start: 73
• Page End: 78
• Publication Date: 2017-09
• Subjects: Guidance law -- Internal model principle -- Adaptive control -- Weaving maneuvering -- Disturbance rejection; Engineering instruments -- Periodicals; Engineering instruments; Periodicals; Electronic journals; 629.805
• DOI: 10.1016/j.isatra.2017.06.006
• Languages: English
• ISSNs: 0019-0578

Abstract

Abstract: For the terminal phase guidance problem of the missile intercepting weaving maneuvering target, an adaptive internal model guidance laws in the three-dimensional (3-D) engagement space is proposed in this paper. The guidance law adopts the disturbance rejection theory by treating the target weaving maneuvering accelerations as external disturbance, which comprises of nominal part and adaptive part. The nominal part based on feedback linearization method ensures the whole guidance system stable and the adaptive part based on internal model principle is used to recover the disturbance signals on-line to reject the target maneuver asymptotically. The algorithm guarantees the whole guidance system with satisfying performance both in transient and steady state on the effect of target maneuver on guidance system. The stability analyses and theory proof are provided in this paper. At last, numerical simulations are carried out to illustrate the effectiveness of the proposed guidance law.