Synonyme wurden verwendet für: State State Estimation
Suche ohne Synonyme: title: Optimal and Robust State Estimation

1–4 von 4 Ergebnissen
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    Gust Load Alleviation Control and Gust Estimation for a High Aspect Ratio Wing Wind Tunnel Model

    Christopher Forte / Nhan Nguyen / Juntao Xiong | NTRS
    response. Then, the reduced model was used to design an extended-state Kalman filter which estimates the states and the sinusoidal gust input. The ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance , Mathematical And Computer Sciences (General)

      Gust Load Alleviation Control and Gust Estimation for a High Aspect Ratio Wing Wind Tunnel Model

      Christopher Forte / Nhan Nguyen / Juntao Xiong | NTRS
      response. Then, the reduced model is used to design an extended-state Kalman filter which estimates the states and the sinusoidal gust input. The ...
      Verlag: NASA National Aeronautics and Space Administration
      Schlagwörter: Aircraft Design, Testing And Performance , Mathematical And Computer Sciences (General)

    Self-tuning control of attitude and momentum management for the Space Station

    Shieh, L. S. / Sunkel, J. W. / Yuan, Z. Z. et al. | NTRS | 1992
    attitude and momentum management for the Space Station. This new hybrid adaptive control scheme combines an on-line recursive estimation algorithm ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance

    Relative Navigation for Formation Flying of Spacecraft

    Alonso, Roberto / Du, Ju-Young / Hughes, Declan et al. | NTRS | 2001
    This paper presents a robust and efficient approach for relative navigation and attitude estimation of spacecraft flying in formation. This ...
    Verlag: NASA National Aeronautics and Space Administration

    Cislunar Near Rectilinear Halo Orbit for Human Space Exploration

    Whitley, Ryan / Martinez, Roland / Condon, Gerald et al. | NTRS | 2016
    identified by a set of Keplerian orbit parameters, and a valid epoch specific state vector must be first obtained from a multi-body dynamical model ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Lunar And Planetary Science And Exploration