CIRCULATORY STRESS IN FLYING FIGHTER AIRCRAFT

被引：0
|
作者：
PIRCHER, L
机构：
来源：
SCHWEIZERISCHE MEDIZINISCHE WOCHENSCHRIFT | 1972年 / 102卷 / 12期
关键词：
D O I：
暂无
中图分类号：
R5 [内科学];
学科分类号：
1002 ; 100201 ;
摘要：
引用
收藏
页码：444 / &
相关论文
共 50 条
  • [1] INFLUENCE OF ROLL COMMAND AUGMENTATION SYSTEMS ON FLYING QUALITIES OF FIGHTER AIRCRAFT
    MITCHELL, DG
    HOH, RH
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1984, 7 (01) : 99 - 105
  • [2] Identification of fighter aircraft
    Lindberg, R
    Fredin, P
    SIGNAL PROCESSING, SENSOR FUSION, AND TARGET RECOGNITION VII, 1998, 3374 : 223 - 234
  • [3] CHARACTERISTICS OF FIGHTER AIRCRAFT
    MADELUNG, GO
    JOURNAL OF AIRCRAFT, 1978, 15 (03): : 129 - 133
  • [4] Swarms of UAVs and fighter aircraft
    Trahan, MW
    Wagner, JS
    Stantz, KM
    Gray, PC
    Robinett, R
    SECOND INTERNATIONAL CONFERENCE ON NONLINEAR PROBLEMS IN AVIATION & AEROSPACE VOL 1 AND 2, 1999, : 745 - 752
  • [5] COMPUTER SIZING OF FIGHTER AIRCRAFT
    COEN, PG
    FOSS, WE
    JOURNAL OF AIRCRAFT, 1986, 23 (05): : 353 - 354
  • [6] Guidance systems of fighter aircraft
    Rajanikanth, KN
    Rao, RS
    Subramanyam, PS
    Vohra, A
    DEFENCE SCIENCE JOURNAL, 2005, 55 (03) : 231 - 244
  • [7] NEXT GENERATION OF FIGHTER AIRCRAFT
    REES, J
    WHITAKER, A
    SCIENCE AND TECHNOLOGY, 1968, (82): : 84 - &
  • [8] BETTER IMAGERS FOR FIGHTER AIRCRAFT
    TROY, CT
    PHOTONICS SPECTRA, 1994, 28 (03) : 30 - 31
  • [9] Fighter aircraft gets a lift
    不详
    MECHANICAL ENGINEERING, 1999, 121 (01) : 20 - +
  • [10] Switched Control for a Fighter Aircraft
    Kemer, Emre
    Prempain, Emmanuel
    2014 UKACC INTERNATIONAL CONFERENCE ON CONTROL (CONTROL), 2014, : 110 - 114
12345