Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/231064
Title: Survey of Global-Positioning-System-Based Attitude Determination Algorithms
Authors: Goh, Shu Ting 
Low, Kay-Soon
Keywords: Science & Technology
Technology
Engineering, Aerospace
Instruments & Instrumentation
Engineering
CARRIER PHASE MEASUREMENTS
GPS ANTENNA ATTITUDE
LEAST-SQUARES
NAVIGATION
SATELLITE
DESIGN
FILTER
Issue Date: 1-Jun-2017
Publisher: AMER INST AERONAUTICS ASTRONAUTICS
Citation: Goh, Shu Ting, Low, Kay-Soon (2017-06-01). Survey of Global-Positioning-System-Based Attitude Determination Algorithms. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 40 (6) : 1321-1335. ScholarBank@NUS Repository.
Abstract: The phase quartic algorithm and attitude-lean-loping estimator with GPS recursive operations (ALLEGRO) have been proposed in a study. Both of these algorithms demonstrate a high rate of error convergence. The phase quartic is an eigenvalue-based estimation algorithm, whereas ALLEGRO is derived based on the minimal model error estimation algorithm. The quaternion vector has been used as the primary attitude representation, except for direction computational matrix (DCM) and attitude matrix solution (AMES) methods. The DCM uses Euler angles, whereas AMES uses nine elements of the attitude matrix as the attitude representation. This study focuses mainly on the existing real-time GPS-based attitude determination methods that are feasible for space application.
Source Title: JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
URI: https://scholarbank.nus.edu.sg/handle/10635/231064
ISSN: 0731-5090
1533-3884
Appears in Collections:Staff Publications
Elements

Show full item record
Files in This Item:
File Description SizeFormatAccess SettingsVersion 
2017_aiaa_gpsurvey.pdfSubmitted version474.39 kBAdobe PDF

OPEN

NoneView/Download

Page view(s)

19
checked on Sep 29, 2022

Download(s)

2
checked on Sep 29, 2022

Google ScholarTM

Check


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.