1 |
V. E. Haloulakos, "Thrust and impulse requirements for jet attitude-control systems," Journal of Spacecraft, p84-90, 1964.
|
2 |
M. H. Kaplan, Modern Spacecraft Dynamics and Control, John Wiley & Sons, New York, pp.261, 1976.
|
3 |
S. J. Dodds, " A predicted signed switching time high precision satellite attitude control law," INT. J. CONTROL, p1051-1061, 1984.
|
4 |
V. E. Haloulakos, " Analysis of jet attitude control systems subject to varying magnitudes of external disturbing torques," AIAA, Guidance, Control and Flight Dynamics Conference, Huntsuille, ALA, pp. 1-11, 1967.
|
5 |
Sang-woon Jeon and Seul Jung, "Novel analysis of limit cycle for PWM signal of PD control system," IEICE electron. Expr., vol. 6, no. 11, pp787-793, 2009.
DOI
|
6 |
B. F. Wu, J. W. Perng, and J. I. Chin, "Limit cycle analysis of nonlinear sampled-data systems by gain-phase margin approach," J. Franklin Inst., vol. 342, pp. 175-192, 2005.
DOI
ScienceOn
|
7 |
Sang-woon Jeon and Seul Jung, " Hardware-in-the-loop simulation for the reaction control system using PWM-based limit cycle Analysis," IEEE Transactions on control systems technology, vol. 20, no 2, 2012.
|
8 |
S. Jeon, J. Kim, and H. Choi, "Development of a thrust measurement system," WASET issue 63, pp. 494-498, March 2012.
|
9 |
Veronika R. Meyer, "Review Measurement uncertainty," Journal of Chromatography A, 1158, pp. 15-24, 2007.
DOI
ScienceOn
|