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Volumn 59, Issue 1, 2006, Pages 119-133

Flight test of attitude determination system using multiple GPS antennae

Author keywords

Ambiguity resolution; Attitude determination; GPS antennae; UAV

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; DOPPLER EFFECT; FLIGHT SIMULATORS; GLOBAL POSITIONING SYSTEM; NAVIGATION SYSTEMS; RADIO RECEIVERS; UNMANNED VEHICLES; WIND EFFECTS;

EID: 31144456686     PISSN: 03734633     EISSN: 14697785     Source Type: Journal    
DOI: 10.1017/S0373463305003498     Document Type: Article
Times cited : (18)

References (13)
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    • The study of real-timed GPS navigation accuracy during approach and landing of an ultralight vehicle
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    • Hsiao, F., Huang, S. and Lee, M. (2003). The study of real-timed GPS navigation accuracy during approach and landing of an ultralight vehicle. Proceedings of International Conference on Recent Advances in Space Technologies, 2003. RAST '03, IEEE, Istanbul, Turkey.
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  • 7
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    • Efficient Attitude Determination Algorithm using Geometrical Concept: SNUGLAD
    • Anaheim, California, January 22-24
    • Kee, C., Jang, J. and Sohn, Y. (2003). Efficient Attitude Determination Algorithm using Geometrical Concept: SNUGLAD. 2003 National Technical Meeting Proceedings, Anaheim, California, January 22-24.
    • (2003) 2003 National Technical Meeting Proceedings
    • Kee, C.1    Jang, J.2    Sohn, Y.3
  • 8
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    • The Impact of GPS Velocity Based Flight Control on Flight Instrumentation Architecture
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  • 9
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    • Flight Test Results of UAV Automatic Control Using a Single-Antenna GPS Receiver
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    • Lee, S., Lee, T., Park, S. and Kee, C. (2003). Flight Test Results of UAV Automatic Control Using a Single-Antenna GPS Receiver, AIAA GN&C Conference and Exhibit, 2003, AIAA-2003-5593.
    • (2003) AIAA GN&C Conference and Exhibit
    • Lee, S.1    Lee, T.2    Park, S.3    Kee, C.4
  • 10
    • 0017981685 scopus 로고
    • Computing Integrals Involving Matrix Exponential
    • June
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  • 11
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    • Development of a Low-cost GPS based Attitude Determination System
    • M.Sc. thesis, Department of Geometrics Engineering Report No. 20175, University of Calgary
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    • Development of an Integrated Low-Cost GPS/Rate Gyro System for Attitude Determination
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    • Wang, C.1    Lachapelle, G.2    Cannon, M.E.3
  • 13
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    • Maintaining high accuracy GPS positioning 'on the fly'
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.