[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 4: 14 - 16

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.04.042

MISSILES AND GUIDANCE TECHNOLOGY

A New Air Data Attitude and Heading Reference System Algorithm Applied to High-dynamic Guidance Flight

  • ZHU Shaohua ,
  • WANG Fang ,
  • GUO Zhixiang ,
  • LEI Hongjie
Expand
  • Flight Automatic Control Research Institute, Xi'an 710065, China

Received date: 2010-12-23

  Online published: 2025-05-30

Fold

Abstract

To promote the availability of attitude and heading reference system (AHRS) for high dynamic guidance flight, a new algorithm of ADAHRS (air data AHRS) based on self-adaptive Kalman filter was presented, the air data was used to eliminate the movement acceleration from the measurement, and the problem of attitude correction and heading in high-dynamic guidance flight was solved. The algorithm is designed and applied to MEMS system. The result of vehicle-borne proves that the algorithm is reasonable, feasible and robust to be applied to missile or aircraft with high maneuver.

Key words： attitude and heading reference system; high-dynamic flight; self-adaptive Kalman filter; MEMS

Cite this article

ZHU Shaohua , WANG Fang , GUO Zhixiang , LEI Hongjie . A New Air Data Attitude and Heading Reference System Algorithm Applied to High-dynamic Guidance Flight[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(4) : 14 -16 . DOI: 10.15892/j.cnki.djzdxb.2011.04.042

[an error occurred while processing this directive]

References

[1]
汪芳, 朱少华, 雷宏杰. 基于卡尔曼滤波器的数字式捷联航姿系统算法设计[J]. 中国惯性技术学报, 2008, 16(2): 208-211.
[2]
Roger C Hayward, J David Powell. Design of multi-sensor attitude determination system[J]. IEEE Transactions on Aerospace and Electronic Systems, 2004, 40(2): 627-649.
[3]
Gebre-Egziabher D, Hayward R C, Powell J D. A low-cost GPS/inertial attitude heading reference system (AHRS) for general aviation applications[C]// IEEE1998 PLANS, 1998: 518-525.
[4]
A K Barrows, Demoz Gebre-Egziabher, Hayward R, et al. GPS-based attitude and guidance displays for general aviation[C]// EFTA'96. Proceedings, 1996: 423-428.
[5]
Sage A P, Husa G W. Adaptive filtering with unknown prior statistics[C]// Proceedings of Joint Automatic Control Conference, 1969: 760-769.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]