1–20 of 58 hits
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    AIAA-2002-4463 Angular Rate Estimation for Gyroless Satellite Attitude Control

    Agrawal, B. / Palermo, W. / AIAA | British Library Conference Proceedings | 2002

    AIAA-2002-4656 Method of Slewing the Spacecraft to Minimize Settling Time

    Agrawal, B. / Chen, H. / AIAA | British Library Conference Proceedings | 2002

    Numerical simulation of inflatable membrane structures

    Kolar, R. / Whittinghill, C. / Agrawal, B. | Tema Archive | 2001

    AIAA-2004-5386 Attitude Determination for NPS Three-Axis Spacecraft Simulator

    Kim, J. / Cristi, R. / Agrawal, B. | British Library Conference Proceedings | 2004

    Cooperative Control of Multiple Space Manipulators

    Yale, G. / Agrawal, B. / AIAA | British Library Conference Proceedings | 1994

    Slew Maneuver of a Flexible Spacecraft Using On/Off Thrusters

    Agrawal, B. / Bang, H. / AIAA | British Library Conference Proceedings | 1993

    Application of Constraint Dynamics for Spacecraft Maneuver

    Bang, H. / Agrawal, B. / AIAA | British Library Conference Proceedings | 1994

    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

    Analysis of Intelsat V flight data

    RUSH, T. / SCHRANTZ, P. / AGRAWAL, B. | AIAA | 1987

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

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

    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