Reducing the negative effects of flywheel disturbance on space camera image quality using the vibration isolation method
Changcheng DENG, Deqiang MU, Junli GUO, Peng XIE
Reducing the negative effects of flywheel disturbance on space camera image quality using the vibration isolation method
Although the performance of space cameras has largely improved, the micro vibration from flywheel disturbances still significantly affects the image quality of these cameras. This study adopted a passive isolation method to reduce the negative effect of flywheel disturbance on image quality. A metal-rubber shock absorber was designed and installed in a real satellite. A finite element model of an entire satellite was constructed, and a transient analysis was conducted afterward. The change in the modulate transfer function was detected using ray tracing and optical transfer function formulas. Experiments based on real products were performed to validate the influence of the metal-rubber shock absorber. The experimental results confirmed the simulation results by showing that the negative effects of flywheel disturbance on the image quality of space cameras can be diminished significantly using the vibration isolation method.
micro vibration / modulate transfer function / vibration isolation / flywheel disturbance
[1] |
Pang S, Yang L, Qu G. New development of micro-vibration integrated modeling and assessment technology for high performance spacecraft. Structure & Environment Engineering, 2007, 34(6): 1–9
|
[2] |
Zhong W C. Spacecraft obit and attitude parameters impact analysis for optical imaging. Dissertation for the Master Degree. Haerbin: Harbin Institute of Technology, 2009
|
[3] |
Lee D O, Yoon J S, Han J H. Development of integrated simulation tool for jitter analysis. International Journal of Aeronautical and Space Sciences, 2012, 13(1): 64–73
CrossRef
Google scholar
|
[4] |
Masterson R A, Miller D W, Grogan R L. Development and validation of reaction wheel disturbance models:empirical model. Journal of Sound and Vibration, 2002, 249(3): 575–598
CrossRef
Google scholar
|
[5] |
Han X. Satellite jitter analysis based on unbalance of flywheel. Aerospace Shanghai, 2012, 29(6): 42–45
|
[6] |
Zhang B, Wang X, Hu Y. Integrated analysis on effect of micro-vibration on high resolution space camera imaging. Spacecraft Recovery & Remote Sensing, 2012, 33(2): 60–66
|
[7] |
Wang H, Wang W, Wang X, Zou G, Li G, Fan X. Space camera image degradation induced by satellite micro-vibration. Acta Photoning Sinica, 2013, 42(10): 1212–1217
CrossRef
Google scholar
|
[8] |
Stewart D. A platform with six degree of freedom. Proceedings-Institution of Mechanical Engineers, 1965, 180(1): 371–386
CrossRef
Google scholar
|
[9] |
Klenke S, Baca T. Structural dynamics test simulation and optimization for aerospace components. Expert Systems with Applications, 1996, 11(4): 82–89
|
[10] |
Rudoler S, Hadar O, Fisher M, Kopeika N S. Image resolution limits resulting from mechanical vibration. Optics and Precision Engineering, 1991, 30(5): 577–589
CrossRef
Google scholar
|
[11] |
Fu M, Liu Y, Cui M, Cao M. Metal-rubber vibration absorber for aerocraft. Optics and Precision Engineering, 2013, 21(5): 1174–1182
CrossRef
Google scholar
|
[12] |
Wang J.Evaluation and optimization on dynamic imaging quality of an optical remote sensor. Dissertation for the Doctoral Degree. Changchun: Changchun Institute of Optics, Fine Mechanics and Physics, 2000
|
[13] |
Zhang Y. Imaging MTF of space camera under vibration and simulation. Optics and Precision Engineering, 2011, 19(9): 2146–2153
CrossRef
Google scholar
|
[14] |
Schowengerdt R A, Basedow R W, Colwell J E. Measurement of the HYDICE system MTF from flight imagery. SPIE Proceedings, 1996, 2821: 127–136
|
[15] |
Léger D, Duffaut J, Robinet F. MTF measurement using spotlight. IEEE Proceedings of IGARRS, 1994, 4: 2010–2012
|
[16] |
Liu C, Jing X, Daley S, Li F. Recent advances in micro-vibration isolation. Mechanical Systems and Signal Processing, 2015, 56–57: 55–80
CrossRef
Google scholar
|
/
〈 | 〉 |