Optimal integrated attitude and state estimation for lunar descent to landing navigation

被引：0
|
作者：
Zanetti, Renato [1 ]
Bishop, Robert H. [2 ]
机构：
[1] Charles Stark Draper Lab Inc, GN&C Manned Space Syste, Cambridge, MA 02139 USA
[2] Univ Texas Austin, Dept Aerosp Engn & Engn Mech, Austin, TX 78712 USA
来源：
SPACEFLIGHT MECHANICS 2008, VOL 130, PTS 1 AND 2 | 2008年 / 130卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Conditions on the optimality of the introduction of preprocessed attitude estimates in the Kalman filter are developed. The results are applied to lunar descent to landing navigation. The attitude estimate is obtained with the Davenport q-method and a modified measurement model. Together with the attitude estimate, the preprocessor passes to the Kalman filter the estimation error covariance.
引用
收藏
页码：995 / +
页数：4
相关论文
共 50 条
  • [21] Application of USQUE based on PSO in attitude estimation of integrated navigation
    Lyu X.
    Hu B.
    Dai Y.
    Zhao R.
    1600, Chinese Institute of Electronics (42): : 1366 - 1371
  • [22] Integrated Simulation and State Estimation for Precision Landing on Titan
    Schutte, Aaron
    Delaune, Jeff
    Skylanskiy, Evgeniy
    Hewitt, Robert
    Daftry, Shreyansh
    Quadrelli, Marco B.
    Matthies, Larry
    2020 IEEE AEROSPACE CONFERENCE (AEROCONF 2020), 2020,
  • [23] Fuel-optimal G-MPSP Guidance for Powered Descent Phase of Soft Lunar Landing
    Sachan, Kapil
    Padhi, Radhakant
    2015 IEEE CONFERENCE ON CONTROL AND APPLICATIONS (CCA 2015), 2015, : 924 - 929
  • [24] INFLUENCE OF SUBOPTIMAL NAVIGATION FILTER DESIGN ON LUNAR LANDING NAVIGATION ACCURACY
    TUCKNESS, DG
    JOURNAL OF SPACECRAFT AND ROCKETS, 1995, 32 (02) : 353 - 359
  • [25] Vision-based absolute navigation for descent and landing
    Van Pham, Bach
    Lacroix, Simon
    Devy, Michel
    JOURNAL OF FIELD ROBOTICS, 2012, 29 (04) : 627 - 647
  • [26] 3-Dimensional advanced solution for lunar descent and landing
    Mehedi, Ibrahim Mustafa
    Kubota, Takashi
    Al-Saggaf, Ubaid M.
    JOURNAL OF VIBROENGINEERING, 2015, 17 (01) : 527 - 543
  • [27] Descent image based landing area terrain reconstruction technology for lunar landing mission
    Li, M.
    Liu, S.
    Ma, Y.
    Sun, C.
    Jia, Y.
    IMAGING SCIENCE JOURNAL, 2015, 63 (08): : 440 - 446
  • [28] Autonomous navigation and guidance for pinpoint lunar soft landing
    Huang, Xiangyu
    Wang, Dayi
    2007 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS, VOLS 1-5, 2007, : 1148 - 1153
  • [29] Guidance, navigation, control of SELENE lunar landing mission
    Kawakatsu, Y
    Kinoshita, T
    Takizawa, Y
    SECOND INTERNATIONAL CONFERENCE ON NONLINEAR PROBLEMS IN AVIATION & AEROSPACE VOL 1 AND 2, 1999, : 349 - 356
  • [30] Variable-Time-Domain Neighboring Optimal Guidance, Part 2: Application to Lunar Descent and Soft Landing
    Mauro Pontani
    Giampaolo Cecchetti
    Paolo Teofilatto
    Journal of Optimization Theory and Applications, 2015, 166 : 93 - 114
12345