1. Optimal feedback gains for three-dimensional large angle slewing of spacecraft;Banerjee;Journal of Guidance, Control and Dynamics,1991
2. SUMO: Spacecraft for universal modification of orbits;Bosse;Proc. SPIE,2004
3. Applied Optimal Control;Bryson,1975
4. J.R. Cloutier, C.N. D'Souza, C.P. Mracek, Nonlinear regulation and nonlinear H∞ control via the state-dependent Riccati equation technique, in: Proc. 1st International Conference on Nonlinear Problems in Aviation and Aerospace, vol. 1, AIAA, Reston, VA, 1996, pp. 117–123.