A Satellite Attitude Determination Algorithm Based on Four-Mode Differential Laser Gyro and Star Sensor

ZANG Qiang; GAO Jing-min; YANG Hong-bo; GUAN Xin; CHEN Shou-lei

doi:10.3969/j.issn.1671-637x.2016.03.020

Journals >Electronics Optics & Control >Volume 23 >Issue 3 >Page 87 > Article

Electronics Optics & Control
Vol. 23, Issue 3, 87 (2016)

A Satellite Attitude Determination Algorithm Based on Four-Mode Differential Laser Gyro and Star Sensor

ZANG Qiang¹, GAO Jing-min¹, YANG Hong-bo¹, GUAN Xin², and CHEN Shou-lei²

Author Affiliations

¹[in Chinese]

²[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2016.03.020 Cite this Article

ZANG Qiang, GAO Jing-min, YANG Hong-bo, GUAN Xin, CHEN Shou-lei. A Satellite Attitude Determination Algorithm Based on Four-Mode Differential Laser Gyro and Star Sensor[J]. Electronics Optics & Control, 2016, 23(3): 87 Copy Citation Text

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References

[3] TAKANORI I.High-bandwidth attitude determination using jitter measurements and optimal filtering［C］//AIAA Gui-dance, Navigation, and Control Conference, Chicago:American Institute of Aeronautics and Astronautics, 2009:14-21.

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