SYSTEM IDENTIFICATION OF AIRCRAFT LONGITUDINAL MOTION UTILIZINGFLIGHT SIMULATOR DATA

被引:0
|
作者
Metodiev, Konstantin [1 ]
机构
[1] Bulgarian Acad Sci, Space Res & Technol Inst, Sofia, Bulgaria
来源
关键词
FlightGear; System Identification; !text type='JS']JS[!/text]BSim; Pilatus PC-9M;
D O I
10.3897/arb.v36.e10
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In the presentedarticle, an exemplaryproblemof identifying the parameters of an aircraft's motion withinthe vertical plane of symmetry is solved. The data was collected by FlightGear simulator for a Pilatus PC-9M aircraft flight case. After submittingasequence of commands to pitch elevatorand engine thrust, the simulator records fiveparameters of longitudinalmotionatacertain frequency. The collected data are further used to build a state-space model of theflightthrough least-squares estimation. The obtained numerical results are compared with theexperimental ones and are overlaid graphically.Charts depicting elevator angle to trim arealsoderived.A source code developed inGNU Octave wasapplied,andthe problemwas solved.
引用
收藏
页数:226
相关论文
共 50 条
  • [21] Structured H∞ control for an aircraft longitudinal motion
    Pang A.-P.
    Zhou H.-B.
    Yang J.
    Yang, Jing, 1600, Editorial Department of Electric Machines and Control (24): : 139 - 143
  • [22] Delay system identification applied to the longitudinal flight of an aircraft through a vertical gust
    Veysset, Francois
    Belkoura, Lotfi
    Coton, Patricia
    Richard, Jean-Pierre
    PROCEEDINGS OF 2006 MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION, VOLS 1 AND 2, 2006, : 306 - +
  • [23] Enhancement of light aircraft 6 DOF simulation using flight test data in longitudinal motion
    Nguyen, L. V. T.
    Tyan, M.
    Lee, J-W
    Kim, S.
    AERONAUTICAL JOURNAL, 2021, 125 (1290): : 1358 - 1379
  • [24] Motion Equations and Longitudinal Control of a Convertible VTOL Aircraft
    Czyba, Roman
    Kronhof, Grzegorz
    2020 7TH INTERNATIONAL CONFERENCE ON CONTROL, DECISION AND INFORMATION TECHNOLOGIES (CODIT'20), VOL 1, 2020, : 1029 - 1034
  • [25] Performance Identification and Compensation of Simulator Motion Cueing Delays
    Fang, Zhou
    Reymond, Gilles
    Kemeny, Andras
    JOURNAL OF COMPUTING AND INFORMATION SCIENCE IN ENGINEERING, 2011, 11 (04)
  • [26] Structural Identification of Dynamic Simulator of UAV Angular Motion
    Ermolaeva, O. V.
    Prokofieva, I. Yu.
    2015 IEEE 3RD INTERNATIONAL CONFERENCE ACTUAL PROBLEMS OF UNMANNED AERIAL VEHICLES DEVELOPMENTS (APUAVD), 2015, : 116 - 119
  • [27] System Identification using in situ experimental data for the development of an Hexapod Surfing Simulator
    Lestrade, Kevin
    Guerard, Sandra
    Lanusse, Patrick
    Viot, Philippe
    2015 IEEE CONFERENCE ON CONTROL AND APPLICATIONS (CCA 2015), 2015, : 453 - 458
  • [28] Neural Network Semi-empirical Modeling of the Longitudinal Motion for Maneuverable Aircraft and Identification of Its Aerodynamic Characteristics
    Egorchev, Mikhail
    Tiumentsev, Yury
    ADVANCES IN NEURAL COMPUTATION, MACHINE LEARNING, AND COGNITIVE RESEARCH, 2018, 736 : 65 - 71
  • [29] Data Processing in the Pilot Training Process on the Integrated Aircraft Simulator
    Hryshchenko, Yurii
    Zaliskyi, Maksym
    Pavlova, Svitlana
    Solomentsev, Oleksandr
    Fursenko, Tatiana
    ELECTRICAL CONTROL AND COMMUNICATION ENGINEERING, 2021, 17 (01) : 67 - 76
  • [30] Simulations and Analysis on Performance Limitations of Aircraft's Longitudinal Motion
    Lu, Di
    Fan, Guoliang
    Yi, Jianqiang
    2010 INTERNATIONAL COLLOQUIUM ON COMPUTING, COMMUNICATION, CONTROL, AND MANAGEMENT (CCCM2010), VOL III, 2010, : 469 - 472