Technical Papers
Oct 15, 2015

Bank-to-Turn Guidance Law with Terminal Impact-Angle Constraint

Publication: Journal of Aerospace Engineering
Volume 29, Issue 3

Abstract

To 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.

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Acknowledgments

The authors are grateful to Prof. Qi Zai-kang for discussions. They would also like to thank the anonymous reviewers for their critical and constructive review of the manuscript. This study was co-supported by the Chinese Postdoctoral Science Foundation 1st Subsidy and Special Subsidy (Grant Nos: 2011M00006 and 2012T50048).

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Information & Authors

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 29Issue 3May 2016

History

Received: Nov 15, 2013
Accepted: Jul 20, 2015
Published online: Oct 15, 2015
Discussion open until: Mar 15, 2016
Published in print: May 1, 2016

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Authors

Affiliations

Lecturer, Dept. of Aerospace, Beijing Institute of Technology, Zhongguanchun South St., Beijing 100081, P.R.China (corresponding author). E-mail: [email protected]
Xia Qunli
Assistant Professor, Dept. of Aerospace, Beijing Institute of Technology, Zhongguanchun South St., Beijing 100081, P.R.China.
Su Weixia
Senior Research Engineer, Beijing Institute of Mechanical Equipment, Yongding St., Beijing 100039, P.R.China.

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