Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization
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Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-16-0439-3_3
Reference35 articles.
1. Zhu, S.Q., Wang, D.W., Shen, Q., Poh, E.K. (2017) Satellite attitude stabilization control with actuator faults. Journal of Guidance Control and Dynamics 40(5): 1–11
2. Sun, L., Zheng, Z.W. (2017) Disturbance observer-based robust backstepping attitude stabilization of spacecraft under input saturation and measurement uncertainty. IEEE Transactions on Industrial Electronics 64(10): 7994–8002
3. Hu, Q.L., Jiang, B.Y., Zhang, Y.M. (2017) Observer-based output feedback attitude stabilization for spacecraft with finite-time convergence. IEEE Transactions on Control Systems Technology 27(2): 781–789
4. Schaub, H., Lappas, V.J. (2009) Redundant reaction wheel torque distribution yielding instantaneous l2 power optimal attitude control. Journal of Guidance, Control, and Dynamics 32(4): 1269–1276
5. Boskovic, J.D., Li, S. M., Mehra, R. K. (2004) Robust tracking control design for spacecraft under control input saturation. Journal of Guidance, Control, and Dynamics 27(4): 627–633
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