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Volumn 41, Issue 2, 1994, Pages 159-174

Integrity Monitoring for Precision Approach Using Kinematic GPS and a Ground‐Based Pseudolite

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT LANDING; ERROR COMPENSATION; RADIO TRANSMITTERS; SIGNAL RECEIVERS; TRACKING (POSITION);

EID: 0028442611     PISSN: 00281522     EISSN: 21614296     Source Type: Journal    
DOI: 10.1002/j.2161-4296.1994.tb02569.x     Document Type: Article
Times cited : (10)

References (11)
  • 3
    • 84981583658 scopus 로고
    • International Standards, Recommended Practices and Procedures for Air Navigation Services—Annex 10
    • (1985)
  • 5
    • 84981586371 scopus 로고    scopus 로고
    • Integrity in Cycle Ambiguity Resolution for GPS‐Based Precision Landing, Differential Satellite Navigation Systems (DSNS)‐94, April 18–22, 1994, Royal Institute of Navigation, London, United Kingdom.
    • Pervan, B.S.1    Cohen, C.E.2    Parkinson, B.W.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.