Analysis of Attitude Determination Methods Using GPS Carrier Phase Measurements

Author:

Baroni Leandro1ORCID,Kuga Hélio Koiti2ORCID

Affiliation:

1. Institute of Science, Engineering and Technology, Federal University of Jequitinhonha and Mucuri Valleys (UFVJM), Rua do Cruzeiro, 1, 39803-371 Teófilo Otoni, MG, Brazil

2. Space Mechanics and Control Division (DMC), National Institute for Space Research (INPE), 12227-010 São José dos Campos, SP, Brazil

Abstract

If three or more GPS antennas are mounted properly on a platform and differences of GPS signals measurements are collected simultaneously, the baselines vectors between antennas can be determined and the platform orientation defined by these vectors can be calculated. Thus, the prerequisite for attitude determination technique based on GPS is to calculate baselines between antennas to millimeter level of accuracy. For accurate attitude solutions to be attained, carrier phase double differences are used as main type of measurements. The use of carrier phase measurements leads to the problem of precise determination of the ambiguous integer number of cycles in the initial carrier phase (integer ambiguity). In this work two algorithms (LSAST and LAMBDA) were implemented and tested for ambiguity resolution allowing accurate real-time attitude determination using measurements given by GPS receivers in coupled form. Platform orientation was obtained using quaternions formulation, and the results showed that LSAST method performance is similar to LAMBDA as far as the number of epochs which are necessary to resolve ambiguities is concerned, but with processing time significantly higher. The final result accuracy was similar for both methods, better than 0.1° to 0.2°, when baselines are considered in decoupled form.

Publisher

Hindawi Limited

Subject

General Engineering,General Mathematics

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1. GPS Receiver Position Estimation and DOP Analysis Using a New Form of the Observation Matrix Approximations;Journal of Sensors;2022-09-19

2. Experiences with the GPS in Unstabilized CubeSat;International Journal of Aerospace Engineering;2020-09-26

3. Effect of Nonlinear Baseline Length Constraint on Global Navigation Satellite System Compass: A Theoretical Analysis;Mathematical Problems in Engineering;2020-05-22

4. Cycle Slip Detection and Repair Using an Array of Receivers with Known Geometry for RTK Positioning;2020 IEEE/ION Position, Location and Navigation Symposium (PLANS);2020-04

5. Improvement of RTK Performances Using an Array of Receivers with Known Geometry;Proceedings of the 2020 International Technical Meeting of The Institute of Navigation;2020-02-13

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