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    Kalman Filter Approach for Re-Eentry Predictions o...

    Sharma, R. K. / Anilkumar, A. K. | AIAA | 2005

    Simulation of Some Historical On-Orbit Breakups Using ASSEMBLE Model

    Anilkumar, A. K. / Ananthasayanam, M. R. / Subba Rao, P. | AIAA | 2003

      SIMULATION OF SOME HISTORICAL ON-ORBIT BREAKUPS USING ASSEMBLE MODEL

      Anilkumar, A. K. / Sarabhai, V. / Ananthasayanam, M. R. et al. | British Library Conference Proceedings | 2003

    Evolution and Expansion of the Orbital Debris Scenario based on Constant Gain Kalman Filter Approach

    Ananthasayanam, M. R. / Anilkumar, A. K. / Subba Rao, P. V. | AIAA | 2004

    STATISTICAL ANALYSIS OF THE ORBITAL CHARACTERISTICS OF THE GEO DEBRIS ENVIRONMENT

    Anilkumar, A. K. / Ananthasayanam, M. R. / Rao, P. V. S. et al. | British Library Conference Proceedings | 2005

    Kalman Filter Approach for Re-Entry Predictions of Risk Objects with K-S Element Equations (IAC-05-B6.3.05)

    Sharma, R. K. / Anilkumar, A. K. / American Astronautical Society et al. | British Library Conference Proceedings | 2006

    Evolution and Expansion of the Orbital Debris Scenario based on Constant Gain Kalman Filter Approach (IAC-04-IAA.5.12.1.10)

    Ananthasayanam, M. R. / Anilkumar, A. K. / Rao, P. V. S. et al. | British Library Conference Proceedings | 2005

    A Proposed Reference Collision Probability Estimation Model of the Space Debris Scenario (IAC-04-IAA.5.12.5.05)

    Anilkumar, A. K. / Ananthasayanam, M. R. / Rao, P. V. S. et al. | British Library Conference Proceedings | 2005

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