• DocumentCode
    1942286
  • Title

    Maximum-likelihood-based filtering for attitude determination via GPS carrier phase

  • Author

    Peng, H.M. ; Chiang, Y.-T. ; Chang, F.R. ; Wang, L.S.

  • Author_Institution
    Dept. of Electr. Eng., Nat. Taiwan Univ., Taipei, Taiwan
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    480
  • Lastpage
    487
  • Abstract
    A maximum-likelihood-based (ML-based) filter is proposed for attitude determination via the GPS carrier phase observables. The quaternion representation is adopted here to describe the attitude. Hence, the norm constraint on the quaternion should be considered. The ML estimation with Lagrange multipliers can be used to consider simultaneously the evolution equation and the constraint, and to minimize the error covariance matrix. The attitude determination via GPS carrier phase observables is fulfilled in two steps. The first step is the GPS carrier phase ambiguity resolution. After the integer ambiguities being fixed, the ML-based filter is used to determine the optimal attitude. The advantage of adopting the quaternion as the state vector to describe the kinematic behavior is that no singular problems arise. To verify our algorithm, the simulation has been conducted. In the simulation, the white noises are added on the carrier phase observables to assess the performance of the proposed method. The body frame is formed by three non-colinear GPS antennae which are mounted on a platform with two aluminum bars representing the baseline vectors. According to the simulation, our method is sound and effective
  • Keywords
    Global Positioning System; covariance matrices; digital simulation; filtering theory; maximum likelihood estimation; phase estimation; white noise; GPS carrier phase; Lagrange multipliers; MLE; aluminum bars; attitude determination; baseline vectors; carrier phase ambiguity resolution; error covariance matrix minimisation; evolution equation; integer ambiguities; kinematic behavior; maximum-likelihood-based filtering; noncolinear GPS antennas; norm constraint; optimal attitude; quaternion representation; simulation; state vector; white noise; Covariance matrix; Equations; Filtering; Filters; Global Positioning System; Kinematics; Lagrangian functions; Maximum likelihood estimation; Position measurement; Quaternions;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, IEEE 2000
  • Conference_Location
    San Diego, CA
  • Print_ISBN
    0-7803-5872-4
  • Type

    conf

  • DOI
    10.1109/PLANS.2000.838342
  • Filename
    838342