A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles
A guidance law for attacking ground target based on motion camouflage strategy is proposed in this paper. According to the relative position between missile and target, the dual second-order dynamics model is derived. The missile guidance condition is given by analyzing the characteristic of motion...
Main Authors: | Chang-sheng Gao, Jian-qing Li, Wu-xing Jing |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2016-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2016/9218754 |
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