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一种新的无人机偏航航迹计算方法

乔宁 唐文辉 贾新成

空军预警学院学报Issue(6):418-421,4.
空军预警学院学报Issue(6):418-421,4.DOI:10.3969/j.issn.2095-5839.2014.06.008

一种新的无人机偏航航迹计算方法

Novel computation method for off-course track of UAV

乔宁 1唐文辉 1贾新成2

作者信息

  • 1. 空军预警学院,武汉430019
  • 2. 中兵通信科技有限公司,河南新乡453000
  • 折叠

摘要

Abstract

To solve the accuracy deficiency of simulation operational software for the track computation of a certain type of UAV, this paper proposes a novel track computation approach based on the positive and negative solution formula of ellipse. According to geodetic coordinate system and the geodetic datum related principles, the off-course track of UAV is calculated by using the micro-element analytic method, and the longitude and latitude of flying UAV in the state of a small off-course angle and the constant altitude are calculated by reducing the time interval. Test results indicate that the track of UAV under the circumstance of a small off-course angle can be calculated accurately by using this algorithm, and the track be corrected for some special cases when the UAV flying over the maximum point and/or equator, which can be also available for the off-course track computation of other air vehicles.

关键词

航迹模拟/无人机偏航/子午线弧长反解

Key words

track simulation/UAV off-course/inverse solution of meridian arc length

分类

航空航天

引用本文复制引用

乔宁,唐文辉,贾新成..一种新的无人机偏航航迹计算方法[J].空军预警学院学报,2014,(6):418-421,4.

空军预警学院学报

2097-180X

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