31–40 von 92 Ergebnissen
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    Passive and active microvibration control for very high pointing accuracy space systems

    Vaillon, L. / Champetier, C. / Guillaud, V. et al. | Tema Archiv | 1997
    pointing accuracy platforms, through the design, prototyping and experimental validation of four microvibration control systems: - an elastomer ...
    Verlag: ESA Publications , Noordwijk

    Analysis of a CTV reentry navigation concept

    Malthan, H. / Fraile-Ordonez, J.M. / Krischke, M. | Tema Archiv | 1997
    Re-entry navigation essentially based on GPS and INS has been analyzed and shown to be feasible. Possible problems have been identified in ...
    Verlag: ESA Publications , Noordwijk

    Flight results from the bird onboard navigation system

    Gill, E. / Montenbruck, O. / Montenegro, S. | Tema Archiv | 2003
    spacecraft during pay load image sessions and enables a geocoding of BIRD sensor images on-the-flight. The analysis of the BIRD ONS flight data ...

    Relative GPS navigation implementation for the ATV rendezvous

    Gonnaud, J.L. / Lagarde, L. / Strandmoe, S.E. et al. | Tema Archiv | 2003
    hundreds meters of the final approach to docking, the ATV Guidance and Control uses the relative position and velocity information from the ...
    Schlagwörter: Navigation

    Optimisation of Aerospace System Control with Constraints on Return Trajectories of Spent Elements

    Filatyev, A. / Golikov, A. / Yanova, O. et al. | British Library Conference Proceedings | 2000
    Schlagwörter: spacecraft guidance , navigation , control systems , ESA

    Titan Flagship Mission 3-Degree-of-Freedom Simulation Analysis

    Prince, Jill L. / Powell, R. W. / Lockwood, Mary Kae | NTRS | 2008
    A NASA flagship mission to Titan, the largest moon of Saturn and the only moon in the solar system with a significant atmosphere, has been ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Lunar And Planetary Science And Exploration

    Control Design for a Critical LEO Earth Observation Satellite, Based on GNSS Sensors for Orbit and Attitude Determination

    Llorente, J. S. / Fernandez-Ibarz, J. M. / Del Cura, J. M. et al. | British Library Conference Proceedings | 2000
    Schlagwörter: spacecraft guidance , navigation , control systems , ESA

    Autonomous planetary landing using a lidar sensor: The navigation function

    De Lafontaine, J. | Tema Archiv | 2003
    guidance and control of the Lander to the safe site. The autonomous navigation function is described in some detail. Numerical results, using a ...
    Schlagwörter: Navigation , LIDAR (light detection and ranging)

    Drag-Free Performance of the ST7 Disturbance Reduction System Flight Experiment on the LISA Pathfinder

    Maghami, Peiman G. / O'Donnell, James R. / Hsu, Oscar H. et al. | NTRS | 2017
    spacecraft. LISA Pathfinder launched from Kourou, French Guiana on December 3, 2015. The DRS is tasked to validate two specific technologies ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance , Attitude Control

    Drag-Free Performance of the ST7 Disturbance Reduction System Flight Experiment on the LISA Pathfinder

    Maghami, Peiman / O'Donnell, James, Jr. / Hsu, Oscar et al. | NTRS | 2017
    spacecraft. LISA Pathfinder launched from Kourou, French Guiana on December 3, 2015. The DRS is tasked to validate two specific technologies ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance , Attitude Control