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    Active vibration suppression of a flexible structure using smart material and a modular control patch

    Song, G / Schmidt, S P / Agrawal, B N | SAGE Publications | 2000

    Attitude Dynamics and Control of Bifocal Relay Mirror Spacecraft (AAS 01-418)

    Agrawal, B. N. / Senenko, C. / AAS et al. | British Library Conference Proceedings | 2001

    Evaluation of a Gyroless Spacecraft Attitude Estimation and Control Concept by Numerical Simulation and Ground Based Experimentation

    Romano, M. / Agrawal, B. N. / European Space Agency | British Library Conference Proceedings | 2003

    Acquisition, tracking and pointing control of the Bifocal Relay Mirror Spacecraft

    Romano, M. / Agrawal, B. N. / International Astronautical Federation | British Library Conference Proceedings | 2003

    Use of Variable Speed Control Moment Gyros for a Fine Pointing Dual Line-of-Sight Spacecraft (AAS 03-041)

    Romano, M. / Agrawal, B. N. / American Astronautical Society | British Library Conference Proceedings | 2003

    Active vibration control of a space truss using a lead zirconate titanate stack actuator

    Song, G / Vlattas, J / Johnson, S E et al. | SAGE Publications | 2001

    Neural Network Attitude Control of Flexible Spacecraft

    Huang, T. / Agrawal, B. N. / International Astronomical Federation | British Library Conference Proceedings | 1998

    Payload Pointing and Active Vibration Isolation Using a Hexapod (AAS 03-561)

    Chen, H.-J. / Bishop, R. M. / Agrawal, B. N. et al. | British Library Conference Proceedings | 2004

    Approaches to Matched Basis Function Repetitive Control (AAS 01-369)

    Chen, H.-J. / Longman, R. W. / Agrawal, B. N. et al. | British Library Conference Proceedings | 2001

    Acquisition, Tracking and Pointing of Bifocal Relay Mirror Spacecraft (AAS 03-151)

    Agrawal, B. N. / American Astronautical Society / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003

    Three-Axis Attitude Simulators for Bifocal Relay Mirror Spacecraft (AAS 03-268)

    Agrawal, B. N. / Romano, M. / Martinez, T. et al. | British Library Conference Proceedings | 2003

    Frequency-Domain Clear-Box Disturbance Rejection (AAS 00-105)

    Chen, H.-J. / Agrawal, B. N. / Longman, R. W. et al. | British Library Conference Proceedings | 2000

    Active Vibration Control of a Deploying Appendage Using Piezoceramic Sensors and Actuators - Abstract

    Bang, H. / Agrawal, B. N. / American Astronautical Society| American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1996

    Rejection of Multiple Periodic Disturbances Using MELMS With Disturbance Identification (AAS 01-143)

    Chen, H.-J. / Agrawal, B. N. / Longman, R. W. et al. | British Library Conference Proceedings | 2001

    Rejection of Multiple Periodic Disturbances Using MELMS With Disturbance Identification (AAS 01-143)

    Chen, H.-J. / Agrawal, B. N. / Longman, R. W. et al. | British Library Conference Proceedings | 2001

    Application of Piezoceramics to Vibration Suppression of a Spacecraft Flexible Appendage

    Meyer, J. L. / Harrington, W. B. / Agrawal, B. N. et al. | British Library Conference Proceedings | 1996

    Nonredundant Single-Gimbaled Control Moment Gyroscopes

    Sands, T A | Online Contents | 2012
    Contributors: Agrawal, B N

    Disturbance Identification and Rejection Experiments on an Ultra Quiet Platform (AAS 99-342)

    Edwards, S. G. / Agrawal, B. N. / Phan, M. Q. et al. | British Library Conference Proceedings | 2000

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