[1] Tsuda, Y. and Nakasuka, S., “New Attitude Motion Following Control Algorithm for Capturing Tumbling Object in Space,” Acta Astronautica, Vol. 53, No. 112003, pp. 847–861.
[2] Dutta, A. and Tsiotras, P., “Egalitarian Peer-to-Peer Satellite Refueling Strategy,” Journal of Spacecraft and Rockets, Vol. 45, No. 3, 2008, pp. 608–618.
[3] Matsumoto, S. and et al., “Satellite Capturing Strategy Using Agile Orbital Servicing Vehicle, Hyper-OSV,”Proceedings of the 2002 IEEE International Conference on Robotics & Automation, Washington DC, USA, 2002,pp. 2309–2314.
[4] Oda, M., Kawano, S., Kibe, K. and Yamagata, F., “ETS-7, A Rendezvous Docking and Space Robot Technology Experiment Satellite Result of the Engineering Model Development Work,” Proceedings of the 34th SICE Annual Conference, Hokkaido, Japan, 1995, pp. 1627–1632.
[5] Kasai, T., Oda, M. and Suzuki, T., “Results of the ETS-7 Mission-Rendezvous Docking and Space Robotics Experiment,” Proceedings of the 5th International Symposium on Artificial Intelligence, Robotics and Automation in Space, ESTEC/ESA, Nordwijk, Netherlands, 1999, pp. 299–306.
[6] Whelan, D. A., Adler, E. A., Wilson, S. B. and Roesler, G.M., “DARPA Orbital Express Program: Effecting a Revolution in Space-Based Systems,” Proceedings of the SPIE, San Diego, CA, USA, 2000, pp. 48–56.
[7] Seth, D. P., “Orbital Express: Leading the Way to a New Space Architecture,” Space Core Technology Conference, Colorado Springs, 2002.
[8] Rupp, T., Boge, T., Kiehling, R. and Sellmaier, F., “Flight Dynamics Challenges of the German on Orbit Servicing Mission DEOS,” Proceedings of the 21st International Symposium on Space Flight Dynamics, Toulouse, France, 2009.
[9] Bajodah A. H., “Inertia-Independent Generalized Dynamic Inversion Feedback Control of Spacecraft Attitude Maneuvers,” Acta Astronautica, Vol. 68, No. 11-12, 2011, pp. 1742–1751.
[10] Kim, K. S. and Kim, Y., “Robust Backstepping Control for Slew Maneuver Using Nonlinear Tracking Function,” IEEE Transactions on Control System Technology, Vol. 11, No. 6, 2003, pp. 822-829.
[11] Leeghim, H., Choi, Y. and Bang, H., “Adaptive Attitude Control of Spacecraft Using Neural Networks,” Acta Astronautica, Vol. 64, No. 7-8, 2009, pp. 778–786.
[12] Krishnakumar, K., Rickard, S. and Bartholomew, S.,“Adaptive Neuro-Control for Spacecraft Attitude Control,” Neurocomputing, Vol. 9, No. 2, 1995, pp. 131-148.
[13] Zou, A. M. and Kumar, K. D. “Adaptive Fuzzy Fault-Tolerant Attitude Control of Spacecraft,” Control Engineering Practice, Vol. 19, No. 1, 2011, pp. 10–21.
[14] Ortega, G. and Giron-Sierra, J.M., “Geno-Fuzzy Control in Autonomous Servicing of a Space Station,”Engineering Applications of Artificial Intelligence, Vol.11, No. 3, 1998, pp. 383-400
[15] Lu, K., Xia, Y., Zhu, Z. and Basin, M. V., “Sliding Mode Attitude Tracking of Rigid Spacecraft with Disturbances,” Journal of the Franklin Institute, Vol.349, No. 2, 2012, pp. 413–440.
[16] Lo, S. C. and Chen, Y. P., “Smooth Sliding Mode Control for Spacecraft Attitude Tracking Maneuvers,”Journal of Guidance, Control and Dynamics, Vol. 18, No. 6, 1995, pp. 1345-1349.
[17] Singla, P., Subbarao, K. and Junkins, J., “Adaptive Output Feedback Control for Spacecraft Rendezvous and Docking Under Measurement Uncertainty,” Journal of Guidance, Control and Dynamic, Vol. 29, No. 4, 2006,pp. 892-902
[18] Gennaro, S. D., “Adaptive Robust Tracking for Flexible Spacecraft in Presence of Disturbances,” Journal of Optimization Theory and Applications, Vol. 98, No. 3, 1998, pp 545-568.
[19] Gennaro, S. D., “Active Vibration Suppression in Flexible Spacecraft Attitude Tracking,” Journal of Guidance, Control, and Dynamics, Vol. 21, No. 3, 1998, pp. 400-408.
[20] Erdong, J. and Zhaowei, S., “Robust Attitude Tracking Control of Flexible Spacecraft for Achieving Globally Asymptotic Stability,” International Journal of Robust and Nonlinear Control, Vol. 19, No. 11, 2009, pp. 1201-1223.
[21]Cloutier, J. R., D’Souza, C. N. and Mracek, C. P., “Nonlinear Regulation and Nonlinear H∞ Control via the State-Dependent Riccati Equation Technique,” Proceedings of the 1st International Conference on Nonlinear Problems in Aviation and Aerospace, AIAA, Reston, VA, USA, 1996, pp. 117–123.
[22] Stansbery, D. T. and Cloutier, J. R., “Position and Attitude Control of a Spacecraft Using the State Dependent Riccati Equation Technique,” Proceedings of the American Control Conference, Chicago, IL, 2000.
[23] Xin, M., Balakrishnan, S. N., “Robust State Dependent Riccati Equation Based Spacecraft Attitude Control,” 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno,NV, 2002.
[24] Lither, M. D. and Dubowsky, S., “State, Shape and Parameter Estimation of Space Objects from Range Images,” Proceedings of the 2004 IEEE International Conference on Robotics and Automation, Piscataway, NJ, 2004, pp. 2974-2979.
[25] Schaub, H. and Junkins, J. L, Analytical Mechanics of Space Systems, 2nd Edition, AIAA Education Series, Reston, VA, 2009.
[26] Turner, J. D. and Chun, H. M., “Optimal Distributed Control of a Flexible Spacecraft During a Large-Angle Maneuver,” Journal of Guidance, Control, and Dynamics, Vol. 7, No. 3, 1984, pp. 257-264.
[27] Cloutier, J. R., Stansbery, D. T., “Nonlinear, Hybrid Bank-to-Turn/Skid-to-Turn Missile Autopilot Design,”AIAA Guidance, Navigation, and Control Conference and Exhibit, Montreal, Canada, 2001
[28] Cimen T., “State-Dependent Riccati Equation (SDRE) Control: A Survey,” Proceedings of the 17th IFAC World Congress, Seoul, Korea, 2008, pp. 3761–3775.
[29] Laub, A. J., “A Schur Method for Solving Algebraic Riccati Equations,” IEEE Transaction on Automatic Control, Vol. AC-24, No. 6, 1979, pp. 913–921.
[30] Fonseca Neto, J. V., Abreu, I.S. and Silva, F.N.,“Neural–Genetic Synthesis for State-Space Controllers Based on Linear Quadratic Regulator Design for Eigenstructure Assignment,” IEEE Transaction on Systems, Man, and Cybernetics—Part B: Cybernetics, Vol. 40, No. 2, 2010, pp. 266-285.
[31] Imae, J., Sagami, H., Kobayashi, T. and Zhai, G., “Nonlinear Control Design Method Based on State-Dependent Riccati Equation (SDRE) via Quasi-Newton Method,” 43rd IEEE Conference on Decision and Control, Bahamas, 2004, pp. 2740-2741
[32] Anderson, B. D. O. and Moore, J. B., Optimal Control:Linear Quadratic Methods, Prentice Hall, Englewood Cliffs, New Jersey, 1990.
[33] Slotine, J. E. and Weiping, L., Applied Nonlinear Control, Prentice Hall, Englewood Cliffs, New Jersey,1991.
[34] Chen, T. and Xu, S., “Double Line-of-Sight Measuring Relative Navigation for Spacecraft Autonomous Rendezvous,” Acta Astronautica, Vol. 67, No. 1-2, 2010, pp. 122–134.
[35] Park, C., Guibout, V. and Scheeres, D. J., “Solving Optimal Continuous Thrust Rendezvous Problems with Generating Functions,” Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 2006, pp. 321-331.
[36] Yang, X., Yu, J. and Gao, H., “An Impulse Control Approach to Spacecraft Autonomous Rendezvous Based on Genetic Algorithms,” Neurocomputing, Vol. 77, No. 1, 2012, pp. 189–196.
