DocumentCode :
3006485
Title :
Spectral analysis and parameter selection for BCB attitude maneuver path of flexible spacecraft
Author :
Zhen Yu ; Chenxing Zhong ; Yu Guo
Author_Institution :
Sch. of Autom., Nanjing Univ. of Sci. & Technol., Nanjing, China
fYear :
2013
fDate :
26-28 Aug. 2013
Firstpage :
729
Lastpage :
734
Abstract :
The classical Bang-Coast-Bang path spectrum was analyzed by FFT in order to select the path parameters which were fit for flexible spacecraft attitude maneuver. Spectrum expression of BCB path was derived by means of DFT. The relation between the path parameters and spectrum as well as maneuver time was studied by analyzing the spectral characteristics of BCB path. A selection method of BCB path parameters was proposed. Research results indicate that if the BCB path parameters are selected by the proposed method, it can effectively reduce flexible appendages´ vibration affected by attitude maneuver for rapid maneuver and rapid stabilization. Numerical simulations demonstrate the effectiveness of the method, and it is useful for BCB path parameters selection.
Keywords :
aerospace control; attitude control; discrete Fourier transforms; fast Fourier transforms; path planning; space vehicles; spectral analysis; BCB attitude maneuver path; DFT; FFT; classical bang-coast-bang path spectrum; flexible appendage vibration reduction; flexible spacecraft attitude maneuver; numerical simulations; path parameter selection method; path planning; spectral analysis; spectral characteristic analysis; spectrum expression; Acceleration; Angular velocity; Attitude control; Path planning; Space vehicles; Stability analysis; Vibrations; Bang-Coast-Bang; flexible spacecraft; parameter selection; path planning; spectral analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information and Automation (ICIA), 2013 IEEE International Conference on
Conference_Location :
Yinchuan
Type :
conf
DOI :
10.1109/ICInfA.2013.6720390
Filename :
6720390
Link To Document :
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