[1]
|
M. R. Akella, “Rigid Body Attitude Tracking without Angular Velocity Feed Back,” System & Control Letters, Vol. 42, No. 4, 2001, pp. 321-326.
doi:10.1016/S0167-6911(00)00102-X
|
[2]
|
B. T. Costic, D. M. Dawson, M. S. De Queiroz and V. Kapila, “A Quaternion-Based Adaptive Attitude Tracking Controller without Velocity Measurements,” Proceedings of the 39th IEEE Conference on Decision and Control, Sydeny, Vol. 3, 12-15 December 2000, pp. 2424- 2429.
|
[3]
|
A. El-Gohary, “Optimal Control of the Rotational Motion of a Rigid Body Using Euler Parameters With the Help of Rotor System,” European Journal of Mechanics-A/Solids, Vol. 24, No. 1, 2005, pp. 111-125.
doi:10.1016/j.euromechsol.2004.10.007
|
[4]
|
A. El-Gohary, “New Optimal Control Law for Attitude of a Rigid Body without Angular Velocity Measurements,” Chaos, Solitons & Fractals, Vol. 25, No. 3, 2005, pp. 557-571. doi:10.1016/j.chaos.2004.12.008
|
[5]
|
A. I. El-Gohary and T. S. Tawfik, “Optimal Control of a Rigid Body Motion Using Euler Parameters Without Angular Velocity Measurements,” Mechanics Research Communications, Vol. 37, No. 3, 2010, pp. 354-359.
doi:10.1016/j.mechrescom.2010.02.004
|
[6]
|
H. Schaub and J. L. Junkins, “Stereographic Orientation Parameters For Attitude Dynamics: A Generalization of the Rodrigues Parameters,” Journal of the Astronautical Sciences, Vol. 44, No. 1, 1996, pp. 1-19.
|
[7]
|
G. R. Izzo and L. Pettazzi, “Command Shaping for a Flexible Satellite Platform Controlled by Advanced Fly- Wheels Systems,” Acta Astronautica, Vol. 60, No. 10-11, 2007, pp. 820-827.
|
[8]
|
J. Li, M. Xu, Z. L.Wang and S. M. Wang, “Minimum-Torque Earth off-Nadir Pointing Control of Gravity-Gradient Stabilized Small Satellites,” Tsinghua Science and Technology, Vol. 5, No. 1, 2000, pp. 31-33.
|
[9]
|
N. Krasovskii, “Problem of Stabilization of Controlled Motion,” In: I. G. Malkin, Ed., The Theory of Motion Stability, Nauka, Moscow, 1966, pp. 475-514.
|
[10]
|
F. Lizarralde and J. T. Wen, “Attitude Control without Angular Velocity Measurement: A Passivity Approach,” IEEE transactions on Automatic Control, Vol. 41, No. 3, 1996, pp. 468-472. doi:10.1109/9.486654
|
[11]
|
M. Lovera and A. Astolfib, “Spacecraft Attitude Control Using Magnetic Actuators,” Automatica, Vol. 40, No. 8, 2004, pp. 1405-1414.
doi:10.1016/j.automatica.2004.02.022
|
[12]
|
V. M. Matrosov, “On Stability of Motion,” Journal of Applied Mathematics and Mechanics, Vol. 26, No. 5, 1962, pp. 992-1002.
|
[13]
|
A. Tayebi, “Unit Quaternion Observer Based Attitude Stabilization of a Rigid Spacecraft Without Velocity Measurement,” Proceedings of the 45th IEEE Conference on Decision and Control, San Diego, 13-15 December 2006, pp. 1557-1561.
|
[14]
|
A. Tayebi and S. McGilvray, “Attitude Stabilization of a VTOL Quadrotor Aircraft,” IEEE Transactions on Control Systems Technology, Vol. 14, No. 3, 2006, pp. 562- 571. doi:10.1109/TCST.2006.872519
|
[15]
|
P. Tsiotras, “A Passivity Approach to Attitude Stabilization Using Nonredundant Kinematic Parameterizations,” Proceedings of the 34th Conference on Decision and Control, New Orleans, 13-15 December 1995, pp. 13-15.
|
[16]
|
P. Tsiotras, H. Shen and C. Hall, “Satellite Attitude Control and Power Tracking With Energy/Momentum Wheels,” Journal of Guidance, Control and Dynamics, Vol. 24, No. 1, 2001, pp. 23-34. doi:10.2514/2.4705
|