Developmental test and evaluation of helicopters using a precision differential global positioning system

被引:0
|
作者
Hardesty, M
Metzger, M
Flint, J
Fredrickson, D
机构
来源
AMERICAN HELICOPTER SOCIETY - 53RD ANNUAL FORUM PROCEEDINGS, VOLS 1 AND 2 | 1997年
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Development of new and innovative applications for high precision differential global positioning systems (DGPS) has exploded in the last two years. Real-time three-dimensional accuracy's of under three centimeters and processed position update rates in excess of four hertz, along with position update latencies of under eighty milliseconds are now commercially available. Immediate position information of this high accuracy and rate opens up tremendous possibilities for automated machine control applications. Over the last two years, MDHS has been developing the ''Portable Test Range'', a DGPS based aircraft position and velocity data archiving tool. When required, the system provides the flight crew with three-dimensional guidance and power cues integrated into a simple but highly effective flight director. The Portable Test Range has been used on numerous FAA certification flight test efforts, including noise certification, height-velocity curve development, and Category A profile development. In the Fail of 1996, the Portable Test Range was used as a flight director for a variety of complex landing approach profiles at NASA Crow's Landing airfield. This flight test program allowed for the simultaneous acquisition of laser position data, and was an opportunity to demonstrate the system to FAA, NASA, Army, and John Volpe Department of Transportation Technical Center staff. Certification of the ''Portable Test Range'' for all types of fixed wing and rotary wing flight test activities is ongoing.
引用
收藏
页码:474 / 485
页数:12
相关论文
共 50 条
  • [1] Global positioning system translators for precision test and evaluation
    Thompson, T
    Westerfield, EE
    JOHNS HOPKINS APL TECHNICAL DIGEST, 1998, 19 (04): : 448 - 458
  • [2] Precision alignment of the LIGO 4 km arms using the dual-frequency differential global positioning system
    Althouse, WE
    Hand, SD
    Jones, LK
    Lazzarini, A
    Weiss, R
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2001, 72 (07): : 3086 - 3094
  • [3] Performances evaluation of different open source DEM using Differential Global Positioning System (DGPS)
    Patel, Arun
    Katiyar, S. K.
    Prasad, Vishnu
    EGYPTIAN JOURNAL OF REMOTE SENSING AND SPACE SCIENCES, 2016, 19 (01): : 7 - 16
  • [4] USING OF DIFFERENTIAL GLOBAL POSITIONING SYSTEM (DGPS) IN INSTRUMENT FLYING
    Sabo, Jozef
    Sabova, Janka
    GEOCONFERENCE ON INFORMATICS, GEOINFORMATICS AND REMOTE SENSING, VOL II, 2014, : 661 - 667
  • [5] Possible application of differential global positioning system (DGPS) to harvesting date and precision viticulture
    Stajnko, D.
    Pulko, B.
    Rakun, J.
    AFRICAN JOURNAL OF BIOTECHNOLOGY, 2010, 9 (48): : 8182 - 8191
  • [6] Satellite test of special relativity using the global positioning system
    Wolf, P
    Petit, G
    PHYSICAL REVIEW A, 1997, 56 (06): : 4405 - 4409
  • [7] DIFFERENTIAL OPERATION OF THE GLOBAL POSITIONING SYSTEM
    ENGE, PK
    KALAFUS, RM
    RUANE, MF
    IEEE COMMUNICATIONS MAGAZINE, 1988, 26 (07) : 48 - 60
  • [8] Cycle ambiguity estimation for aircraft precision landing using the global positioning system
    Pervan, BS
    Parkinson, BW
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1997, 20 (04) : 681 - 689
  • [9] Integrated hardware investigations of precision spacecraft rendezvous using the global positioning system
    Ebinuma, T
    Bishop, RH
    Lightsey, EG
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (03) : 425 - 433
  • [10] Monitoring glacier changes using a global positioning system in differential mode
    Jacobsen, FM
    Theakstone, WH
    ANNALS OF GLACIOLOGY, VOL 24, 1997, 1997, 24 : 314 - 319