Simple Guidance Scheme for Low-Thrust Orbit Transfers
Craig A. Kluever
- 发表年份
- 1998
- 引用次数
- 81
摘要
3Pao, L. Y., “Minimum-Time Control Characteristics of Flexible Structures,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 123–129. 4Singh,T., andVadali, S.R., “RobustTime-Optimal Control:AFrequency Domain Approach,” Journal of Guidance, Control, and Dynamics, Vol. 17, No. 2, 1994, pp. 346–353. 5Singer, N. C., and Seering, W. P., “Preshaping Command Inputs to Reduce System Vibration,” Journal of Dynamic Systems, Measurement and Control, Vol. 12, March 1990, pp. 76–82. 6Banerjee, A. K., “Dynamics and Control of the Shuttle-Antennae System,” Journal of the Astronautical Sciences, Vol. 41, Jan.–March, 1993, pp. 73–90. 7Singhose, W., Banerjee, A. K., and Seering, W. E., “Slewing Flexible Spacecraft with De ection Limiting Input Shaping,” Journal of Guidance, Control, and Dynamics, Vol. 20, No. 2, 1997, pp. 291–298. 8Singhose,W., and Singer, N., “Effects of Input Shaping on Two-Dimensional Trajectory Following,” IEEE Transactions on Robotics and Automation, Vol. 12, No. 6, 1996, pp. 881–887. 9Spong,M.W., and Vidyasagar, M., RobotDynamics andControl, Wiley, New York, 1989, pp. 24, 259–283. 10Banerjee, A. K., and Singhose, W. E., “Input Shaping with Nonlinear Tracking Control of a Two-Link Flexible Robot,”AAS/AIAA Astrodynamics Specialist Conf., AAS Paper 97-121, Sun Valley, ID, Aug. 1997.
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