| 机载单站只测向定位最优机动研究 |
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| 引用本文： | 王体明,李彦志,赵利杰.机载单站只测向定位最优机动研究[J].飞机设计,2013(6):33-37. |
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| 作者姓名： | 王体明 李彦志 赵利杰 |
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| 作者单位： | [1]中国人民解放军93846部队,新疆昌吉831112 [2]空军航空大学,吉林长春130022 |
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| 摘 要： | 概述了机载单站只测向定位最优机动求解算法，研究了基于最大方位角变化率准则下的观测机机动轨迹，得到理论上的最优定位机动，并结合实际运用，分析出两种近似最优的机动：“一”形（直线形）机动和S形机动，通过仿真，验证了这2种机动方式在一定条件下可以等效于最优机动，具有良好的定位效果。
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| 关 键 词： | 只测向定位 最大方位角变化率 最优机动 |
A Research on Optimal Maneuver of Airborne Single Observer Bearings-Only System |
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| WANG Ti-ming,LI Yan-zhi,ZHAO Li-jie.A Research on Optimal Maneuver of Airborne Single Observer Bearings-Only System[J].Aircraft Design,2013(6):33-37. |
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| Authors: | WANG Ti-ming LI Yan-zhi ZHAO Li-jie |
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| Institution: | 1. PLA93846, Changji 831112, China) (2. Aviation University for Air Force, Changchun 130022, China) |
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| Abstract: | This paper summarized the optimal maneuver algorithm, researched on optimal maneuver based on maximum bearings rate and find the optimal maneuver trajectory in theory. Combining with practice, it found out two approximate optimal maneuver trajectory： linear maneuver and S maneuver, by simulation experiment, knew that the two maneuver were equivalent to optimal maneuver in a certain condition and had good location effects. |
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| Keywords: | bearings-only system maximum bearings rate optimal maneuver |
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