(Cui G T, Cheng X J. Line-of-sight pointing control of spacecraft considering input saturation[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(3): 644-654.)
[4]
Godard, Kumar K D. Robust attitude stabilization of spacecraft subject to actuator failures[J]. Acta Astronautica, 2011, 68(7/8): 1242-1459.
[5]
Bajodah A H. Singularity perturbed feedback linearization with linear attitude deviation dynamics realization[J]. Nonlinear Dyanmics, 2008, 53(4): 321-343.
[6]
Hall J S. Analysis and experimentation of control strategies for underactuated spacecraft[D]. Department of Mechanical and Astronautical Engineering, Naval Postgraduate School, 2009.
[7]
Wheeler G, Su C, Stepanenko Y. A sliding mode controller with improved adaptation laws for the upper bounds on the norm of uncertainties[J]. Automatica, 1998, 34(12): 1657-1661.
[8]
Kristiansen R, Nicklasson P J. Spacecraft formation flying: A review and new results on state feedback control[J]. Acta Astronautica, 2009, 65(11/12): 1537-1552.
(Tie Y J, Yue X K, Cao J. Nonlinear feed forward control on attitude and orbital coupling model for spacecraft[J]. Chinese Space Science and Technology, 2010, 30(6): 11-16.)
(Zhu Z B, Li G, He Y Z, et al. Relative cooperative attitude and position control of fractioned spacecraft based on iterative optimization[J]. Chinese Space Science and Technology, 2011, 31(2): 1-8.)
(Zhou J K, Hu Q L, Ma G F, et al. Cooperative attitude and translation control of satellite formation flying using consensus algorithm[J]. Systems Engineering and Electronics, 2011, 33(4): 825-832.)
(Wang J Y, Liang H Z, Sun Z W. Dual number-based relative coupled dynamics and control[J]. J of Astronautics, 2010, 31(7): 1711-1717.)
[17]
Xin M, Pan H J. Integrated nonlinear optimal control of spacecraft in proximity operations[J]. Int J of Control, 2010, 83(2): 347-363.
[18]
Wu Y H, Cao X B, Xing Y J, et al. Relative motion coupled control for formation flying spacecraft via convex optimization[J]. Aerospace Science and Technology, 2010, 14(6): 415-428.
[19]
Wang J Y, Liang H Z, Sun Z W, et al. Relative motion coupled control based on dual quaternion[J]. Aerospace Science and Technology, 2013, 25(1): 102-113.
[20]
Wu J J, Liu K, Han D P. Adaptive sliding mode control for six-DOF relative motion of spacecraft with input constraint[J]. Acta Astronautica, 2013, 87(2): 64-76.
(Ge X S, Lv J. Numerical algorithm for the attitude motion planning of an underactuated system of coupled rigid bodies spacecraft[J]. J of Astronautics, 2009, 30(2): 645-651.)
(Chen S, Ge X S. Feasible trajectory generation of an underactuated spacecraft base on differential flatness[J]. J of Beijing Information Science and Technology University, 2010, 25(2): 30-36.)
[27]
Tsiotras P, Luo J. Reduced effort control laws for underactuated rigid spacecraft[J]. J of Guidance Control and Dynamics, 1997, 20(6): 1089-1095.
[28]
Tsiotras P. Feasible trajectory generation for underactuated spacecraft using differential flatness[C]. AAS/AIAA Astrodynamics Specialist Conf. Girdwood, 1999: 1-11.