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contributor authorWen Qiuqiu
contributor authorXia Qunli
contributor authorSu Weixia
date accessioned2017-12-16T09:22:50Z
date available2017-12-16T09:22:50Z
date issued2016
identifier other%28ASCE%29AS.1943-5525.0000552.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4242122
description abstractTo avoid the mathematical singularity of polar converting in bank-to-turn (BTT) guidance and to provide the specified terminal impact angle, a BTT guidance law with impact-angle constraint (BTT-GL/IA) is presented. Considering the influence of the impact-angle control and target maneuver to the miss-distance, a new form zero-effort miss-distance with impact angle (ZEM/IA) is introduced. Referring to the Lyapunov-like approach used to drive the guidance law in the prior literature, a Lyapunov function is constructed in terms of ZEM/IA. Based on the Lyapunov stability theorem, a negative definite function is designed, and the BTT-GL/IA is derived. Next, BTT-GL/IA is implemented in another form with the variables as the line-of-sight angle and its rate, which are easily measured by the seeker. When using BTT-GL/IA, the guidance law tends to maintain smooth and continuously-varied body acceleration and roll-angle commands while satisfying the impact position and angle constraints. The problem of a mathematical singularity in normal BTT polar converting logic is avoided. Finally, both the maneuverable and stationary targets with different impact-angle constraints are considered in numerical simulations. Through various simulation results, the effectiveness and practicality of the BTT-GL/IA are demonstrated.
publisherAmerican Society of Civil Engineers
titleBank-to-Turn Guidance Law with Terminal Impact-Angle Constraint
typeJournal Paper
journal volume29
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000552
treeJournal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 003
contenttypeFulltext


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