Study on Attitude Control Algorithms for Micro-Satellites

LI Li-zhe; LIU Yong; PAN Quan; FENG Qian; FAN Ding

doi:10.3969/j.issn.1671-637x.2014.10.008

[1] LI J Y, WU B F, ZHANG X M.Development of CubeSat and its enlightenment ［J］.Spacecraft Engineering, 2012, 21(3):80-87.

[2] TU S C.Dynamics and control of satellite attitude［M］.Beijing:China Astronautic Publishing House, 1999.

[3] WU Q, SAIF M.Robust fault diagnosis for a satellite large angle attitude system using an Iterative Neuron PID(INPID)observer［C］//Proceedings of the American Control Conference, 2006:5710-5715.

[4] MACKUNIS W, DUPREE K, BHASIN S, et al.Adaptive neural network satellite attitude control in the presence of inertia and CMG actuator uncertainties［C］//American Control Conference, Washington, 2008:2975-2980.

[5] LIU H, GUO L, YANG Z H, et al.Mixed saturating H2/H∞ state-feedback design for microsatellite attitude control［C］//The 29th Chinese Control Conference, Beijing, 2010:6149-6154.

[6] WANG P, SHTESSEL Y B, WANG Y Q.Satellite attitude control using only magnetorquers［C］//IEEE Proceedings of the 30th Southeastern Symposium on System Theory, Virginia, 1998:500-504.

[7] OUSALOO H S, BADPA A.Magnetic attitude control system for spin stabilized satellite［C］//The 20th Iranian Conference on Electrical Engineering, 2005:1029-1034.

[8] LIU H Y, WANG H N, CHENG Y H.Attitute control of micro-satellite with active magnetic control［J］.Journal of Applied Sciences, 2007, 25(4):377-381.

[9] WINIEWSKI R.Linear time-varying approach to satellite attitude control using only magnetic actuation［J］.Journal of Guidance Control and Dynamics, 2000, 23(4).

[10] WISNIEWSKI R, BLANKE M．Fully magnetic attitude control for spacecraft subject to gradient［J］.Automatica, 1999, 35(7):1201-1214．

[11] HAO D, SHENG T, CHEN X Q.Small satellite magne-tism control for velocity damping［C］//The Second International Conference on Digital Manufacturing & Automation, 2011:1105-1110.

[12] HERVAS J R, REYHANOGLU M, DRAKUNOV S V.Three-axis magnetic attitude control algorithms for small satellites in the presence of noise［C］//The 12th International Conference on Control, Automation and Systems (ICCAS), 2012:17-21.

[13] REYHANOGLU M, HERVAS J R.Magnetic attitude control design for small satellites via slowly-varying systems theory［C］//IECON 38th Annual Conference on IEEE Industrial Electronics Society, 2012:25-28.

[14] INAMORI T, SAKO N, NAKASUKA S.Magnetic dipole moment estimation and compensation for an accurate attitude control in nano-satellite missions［J］.Acta Astronautica, 2011, 68(11):2038-2046.

[15] ZHANG R, XIE X H, ZHANG J.Attitute control of micro-satellite based on active magnetic control algorithm［J］.Journal of Astronautics, 2009, 30(1):193-197.