Untwisting Spin Low-Cost Platform Design Used for Strap-Down Inertial Navigation System in High-Speed Spin Flight Vehicle-Reference-Cited by-同舟云学术

Untwisting Spin Low-Cost Platform Design Used for Strap-Down Inertial Navigation System in High-Speed Spin Flight Vehicle

Published:2014 Issue:6 Volume:57 Page:331-335
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

WANG Decheng¹,LIN Hui¹,QI Rong¹

Affiliation:

1. Shaanxi Key Laboratory of Small & Special Electrical Machine and Drive Technology, Automatic School, Northwestern Polytechnical University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/57/6/57_331/_pdf

Reference16 articles.

1. 1) Rong, J., Xu, T. and Li, J.: Modal Analysis of Transverse Vibration of a Spinning Rocket Based on Timoshenko Beam, Trans. Beijing Inst. Technol., 32, 6 (2012), pp. 551-555.

2. 2) Zhang, M., Ma, T., Cao, Y. and Zu, J.: A Navigation System for Spinning Projectile, Acta Armamentarii, 29, 7 (2008), pp. 793-797.

3. 3) Wang, C., Dong, J., Gao, Z., Yang, S. H. and Chen, J.: Attitude Algorithm of High Dynamic Range Single-axis Platform INS on Rocket Projectile, J. Chin. Inertial Technol., 20, 3 (2012), pp. 257-261.

4. 4) Qin, Y.: Inertial Navigation, Science Technology Press, Beijing, 2006.

5. 5) Shi, Y. S., Wang, B., Dong, M. J. and Gao, Z. F.: Research of Roll-isolated Gimbal Platform and a Two-position Initial Alignment Scheme of SINS in Spinning Projectile, Adv. Mater. Res., 383 (2012), pp. 4115-4120.

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