IDENTIFICATION OF THRUST VECTOR EFFECTIVENESS FROM X-31A FLIGHT TEST DATA

被引:0
|
作者
PLAETSCHKE, E
WEISS, S
机构
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
A main feature of the U.S./German post-stall demonstrator X-31A is its thrust vectoring system which provides additional control in the pitch and yaw axes. The effectiveness of this system could be identified from flight test data. After a brief description of the evaluation method, first results are presented.
引用
下载
收藏
页码:235 / 238
页数:4
相关论文
共 50 条
  • [1] X-31A system identification using single-surface excitation at high angles of attack
    Weiss, S
    Friehmelt, H
    Plaetschke, E
    Rohlf, D
    JOURNAL OF AIRCRAFT, 1996, 33 (03): : 485 - 490
  • [2] Identification of Engine Thrust and Aerodynamic Drag Force According to Flight Test Data with Smoothing of Random Measurement Errors
    Korsun, O.N.
    Poplavsky, B.K.
    Stulovskii, A.V.
    Om, Moung Htang
    Journal of Computer and Systems Sciences International, 2024, 63 (03) : 432 - 446
  • [3] PARIS FLIGHT TO CAP BUSY X-31 TEST SCHEDULE
    DORNHEIM, MA
    AVIATION WEEK & SPACE TECHNOLOGY, 1995, 142 (24): : 112 - 112
  • [4] Research on Engine Thrust and Load Factor Prediction by Novel Flight Maneuver Recognition Based on Flight Test Data
    Zhang, Mengchuang
    Xia, Shasha
    Huang, Yongsheng
    Tian, Jiawei
    Yin, Zhiping
    AEROSPACE, 2023, 10 (11)
  • [5] Intelligent support for aircraft flight test data processing in problem of engine thrust estimation
    Korsun, O. N.
    Poplavsky, B. K.
    Prihodko, S. Ju.
    XII INTERNATIONAL SYMPOSIUM INTELLIGENT SYSTEMS 2016, (INTELS 2016), 2017, 103 : 82 - 87
  • [6] IDENTIFICATION OF A COUPLED FLAPPING INFLOW MODEL FOR THE PUMA HELICOPTER FROM FLIGHT TEST DATA
    DUVAL, R
    BRUHIS, O
    GREEN, J
    VERTICA, 1989, 13 (03): : 267 - 280
  • [7] MEASUREMENT OF PILOT DESCRIBING FUNCTIONS FROM FLIGHT TEST DATA WITH AN EXAMPLE FROM GEMINI X
    WINGROVE, RC
    EDWARDS, FG
    IEEE TRANSACTIONS ON MAN-MACHINE SYSTEMS, 1968, MMS9 (03): : 49 - &
  • [8] Global model approach for X-31 VECTOR system identification
    Rohlf, D
    JOURNAL OF AIRCRAFT, 2005, 42 (01): : 54 - 62
  • [9] Application of system identification techniques to tejas flight test data
    Singh, Jatinder
    Saraf, Amitabh
    Patel, Vijay
    Basappa
    Tharewal, Sachin
    International Journal of Aerospace Innovations, 2013, 5 (01) : 11 - 18
  • [10] Evaluation of subspace identification techniques for the analysis of flight test data
    Hermans, L
    Van der Auweraer, H
    Abdelghani, M
    Guillaume, P
    IMAC - PROCEEDINGS OF THE 16TH INTERNATIONAL MODAL ANALYSIS CONFERENCE, VOLS 1 AND 2, 1998, 3243 : 300 - 306