OPTIMAL TAKEOFF PERFORMANCE OF A VECTORED THRUST AIRCRAFT

被引：0
|
作者：
AVANZINI, G
DEMATTEIS, G
机构：
来源：
AERONAUTICAL JOURNAL | 1995年 / 99卷 / 987期
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：
The optimal takeoff performance of a vectored thrust V/Stol aircraft is analysed by a nonlinear programming method based on a sequential unconstrained minimisation technique. The study is focused on ship operations which involve VTO and ski-jump STO launches. Once the optimal ramp geometry is determined, minimum-fuel and minimum-time problems are solved. The optimal control sequences are evaluated and the effects of ship motion and atmospheric winds are discussed. A microburst encounter following an STO launch is also dealt with in terms of aircraft survival.
引用
收藏
页码：275 / 281
页数：7
相关论文
共 50 条
  • [1] Optimal takeoff performance of a vectored thrust aircraft
    Avanzini, G.
    de Matteis, G.
    1600, Royal Aeronautical Soc, London, United Kingdom (99):
  • [2] Transition controller design of thrust-vectored vertical and/or short takeoff and landing aircraft based on single-step optimal method
    Cheng Z.-Q.
    Yuan X.-M.
    Wang X.-Y.
    Zhu J.-H.
    Zhu, Ji-Hong (jhzhu@tsinghua.edu.cn), 1600, Northeast University (35): : 1338 - 1344
  • [3] Nonlinear dynamics of a vectored thrust aircraft
    Sorensen, CB
    Mosekilde, E
    Granasy, P
    PHYSICA SCRIPTA, 1996, T67 : 176 - 183
  • [4] THRUST-VECTORED TAKEOFF, LANDING, AND GROUND HANDLING OF AN AIRSHIP
    NAGABHUSHAN, BL
    TOMLINSON, NP
    JOURNAL OF AIRCRAFT, 1986, 23 (03): : 250 - 256
  • [5] Deceleration transition controller design of thrust-vectored short takeoff and vertical landing aircraft based on control allocation
    Liu L.
    Tang Y.
    Tao C.
    Zhen Z.
    Liu J.
    Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2022, 43 (06): : 832 - 841
  • [6] Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraft
    Zhiqiang CHENG
    Jihong ZHU
    Xiaming YUAN
    Xiangyang WANG
    ScienceChina(InformationSciences), 2021, 64 (03) : 235 - 237
  • [7] Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraft
    Zhiqiang Cheng
    Jihong Zhu
    Xiaming Yuan
    Xiangyang Wang
    Science China Information Sciences, 2021, 64
  • [8] Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraft
    Cheng, Zhiqiang
    Zhu, Jihong
    Yuan, Xiaming
    Wang, Xiangyang
    SCIENCE CHINA-INFORMATION SCIENCES, 2021, 64 (03)
  • [9] The impact of aircraft takeoff thrust setting on NOX emissions
    Koudis, George S.
    Hu, Simon J.
    North, Robin J.
    Majumdar, Arnab
    Stettler, Marc E. J.
    JOURNAL OF AIR TRANSPORT MANAGEMENT, 2017, 65 : 191 - 197
  • [10] Contribution to modeling and identification of a thrust-vectored aircraft
    Friehmelt, Holger
    Forschungsbericht - Deutsche Forschungsanstalt fuer Luft - und Raumfahrt e.V., 1999, 99 (21): : 4 - 175
12345