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Volumn 41, Issue 1, 1994, Pages 83-97

Flight Tests of Attitude Determination Using GPS Compared Against an Inertial Navigation Unit

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ANTENNAS; CARRIER COMMUNICATION; FLIGHT DYNAMICS; INERTIAL NAVIGATION SYSTEMS; INSTRUMENT TESTING; MANEUVERABILITY; PERFORMANCE; POSITION MEASUREMENT; RING LASERS; TURBULENCE;

EID: 0028383252     PISSN: 00281522     EISSN: 21614296     Source Type: Journal    
DOI: 10.1002/j.2161-4296.1994.tb02323.x     Document Type: Article
Times cited : (59)

References (5)
  • 3
    • 84981627757 scopus 로고
    • Aircraft Applications of GPS‐Based Attitude Determination: Test Flights on a Piper Dakota, ION GPS‐92, Albuquerque, NM
    • (1992)
    • Cohen1    Parkinson2
  • 5
    • 84981587595 scopus 로고
    • Two Studies of High Performance Attitude Determination Using GPS: Generalizing Wahba's Problem for High Output Rates and Evaluation of Static Accuracy Using a Theodolite, ION GPS‐92, Albuquerque, NM
    • (1992)
    • Cohen1    Cobb2    Parkinson3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.