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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.

关键词

Thrust vectoringRoboticsLimitingComputer scienceControl theory (sociology)SpacecraftTrajectorySystem dynamicsNonlinear systemControl (management)

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