1998•Journal of Guidance Control and DynamicsRequires access

Simple Guidance Scheme for Low-Thrust Orbit Transfers

Craig A. Kluever

Open publisher page 81 citations

Abstract

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.

About this research paper

What this paper is about

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.

Why it matters

OpenAlex reports 81 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

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.

Key concepts: Thrust vectoring, Robotics, Limiting, Computer science, Control theory (sociology), Spacecraft, Trajectory, System dynamics

Related papers

Back to paper searchBrowse research topicsOriginal source
Simple Guidance Scheme for Low-Thrust Orbit Transfers — Research Paper | ScholarLens