[1]蔡青春,王惠南.单天线GPS接收机载体姿态测定分析[J].南京理工大学学报(自然科学版),2002,(06):585-589.
 CaiQingchun WangHuinan.Attitude Determination with Single-antenna GPS Receiver[J].Journal of Nanjing University of Science and Technology,2002,(06):585-589.
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单天线GPS接收机载体姿态测定分析()
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
期数:
2002年06期
页码:
585-589
栏目:
出版日期:
2002-12-30

文章信息/Info

Title:
Attitude Determination with Single-antenna GPS Receiver
作者:
蔡青春王惠南
南京航空航天大学自动化学院, 南京210016
Author(s):
CaiQingchun WangHuinan
College of Automation,NUAA,Nanjing 210016
关键词:
全球定位系统 单天线 卡而曼滤波 新系姿态
Keywords:
global posit ioning system single-antenna Kalman f ilter pseudo-att itude
分类号:
V249.3
摘要:
该文研究了利用单天线GPS接收机的输出信息来实时确定载体姿态的基本原理与方法。文中的GPS载体姿态是指关于载体飞行速度矢量轴的新系偏航角、航迹角和新系滚转角 ,亦称为新系姿态。文中对姿态测定的分析包括利用GPS接收机配合软件LABMON4 6输出的原始信息来分析速度矢量的求解方案 ;利用卡而曼滤波模型对速度信息进行处理得到相应的加速度信息 ;根据前面 2步求得的速度和加速度给出解算载体新系姿态的方法 ;最后给出常规姿态与新系姿态的关系和对照说明
Abstract:
The principle and method of aircraft att itude determination w ith the information g iven by single-antenna GPS receiver are discussed . The at titude ment ioned in the paper is also called as pseudo-at titude. It consist s of f light path angle to the local horizontal plane and roll ang le about the aircraf t velocity vector ax is. There are four major sect ions in this paper: to achieve the velocity vector by analyzing the information g iven by the GPS receiver; to est imate accelerat ion vector using a Kalman filter model with the velocity vector information; the at t-i tude synthesizing algorithm model; the relat ion and cont rast of t radit ional att itude and pseudoat titude.

参考文献/References:

1 黄圳圭. 航天器姿态动力学. 长沙: 国防科技大学出版社, 1997
2 May M, Nguyen K, Tanju B. On GPS v elocity . In: Richard L G. Proceedings of the 46 th Annual Meeting of the Institute of Navigation. Washington, D. C: Institued of Nav igation, 1990. 176~ 182
3 刘乐善1 微型计算机接口技术原理及应用1 武汉: 华中理工大学出版社, 1996
4 Chaffee J W, Abel J S. The GPS filtering problem. In: Thomase S. IEEE 1992 Position Locat ion and Navig at ion Symposium. New York: Institue o f Electrical and Electronics Engineers, 1992. 10 ~ 20
5 万德钧. GPS 动态滤波的理论、方法及应用. 南京: 江苏科学技术出版, 1996

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 Zhang Zhian,Lei Xiaoyun.Research and realization for increase-resistance-coefficient of whole- course-controllable trajectory correction projectile based on GPS[J].Journal of Nanjing University of Science and Technology,2015,39(06):460.

备注/Memo

备注/Memo:
航空科学基金资助项目 (99E5 2 0 36 )
蔡青春 男 28 岁 助理工程师
更新日期/Last Update: 2002-12-30