Increasing the range of an emergency hypersonic flight trajectory by optimal control of fuel dumping

被引:0
|
作者
Sachs, G [1 ]
Mayrhofer, M [1 ]
机构
[1] Tech Univ Munich, Lehrstuhl Flugmech & Flugregelung, D-85747 Garching, Germany
关键词
D O I
暂无
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
引用
收藏
页码:S775 / S776
页数:2
相关论文
共 46 条
  • [31] Fuzzy Optimal Tracking Control of Hypersonic Flight Vehicles via Single-Network Adaptive Critic Design
    Bu, Xiangwei
    Qi, Qiang
    IEEE TRANSACTIONS ON FUZZY SYSTEMS, 2022, 30 (01) : 270 - 278
  • [32] Optimal control strategy for economy and durability of extended range fuel cell vehicle
    Lü Q.
    Teng T.
    Zhang B.
    Zhang X.
    Xue Q.
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2021, 53 (07): : 126 - 133
  • [33] Flight-Propulsion Integration Dynamic Analysis and Adaptive Control of the Hypersonic Vehicle at Wide-Range Mach Numbers
    Li, Jiaxin
    Li, Danwei
    Wu, Guoqiang
    Liu, Kai
    IEEE ACCESS, 2022, 10 : 6954 - 6965
  • [34] Flight trajectory design in the presence of contrails: Application of a multiphase mixed-integer optimal control approach
    Soler, Manuel
    Zou, Bo
    Hansen, Mark
    TRANSPORTATION RESEARCH PART C-EMERGING TECHNOLOGIES, 2014, 48 : 172 - 194
  • [35] Instationary Heat-Constrained Trajectory Optimization of a Hypersonic Space Vehicle by ODE-PDE-Constrained Optimal Control
    Chudej, Kurt
    Pesch, Hans Josef
    Waechter, Markus
    Sachs, Gottfried
    Le Bras, Florent
    VARIATIONAL ANALYSIS AND AEROSPACE ENGINEERING, 2009, 33 : 127 - +
  • [36] Simplified Optimal Trajectory Control for 1 MHz LLC Converter with Wide Input Voltage Range
    Nabih, Ahmed
    Ahmed, Mohamed
    Li, Qiang
    Lee, Fred C.
    THIRTY-FOURTH ANNUAL IEEE APPLIED POWER ELECTRONICS CONFERENCE AND EXPOSITION (APEC 2019), 2019, : 212 - 219
  • [37] MIXED PRIMAL/DUAL ALGORITHM FOR DEVELOPING LINEAR FUEL-OPTIMAL IMPULSIVE-CONTROL TRAJECTORY
    Kim, Youngkwang
    Park, Sang-Young
    Park, Chandeok
    SPACEFLIGHT MECHANICS 2015, PTS I-III, 2015, 155 : 101 - 117
  • [38] Fuel consumption optimal control of velocity vector for multiengine aircraft over operating range of engine velocities
    Chuprun, B.E.
    Avtomatika i Telemekhanika, 2002, (12): : 41 - 48
  • [39] Reduced-order Linear Extended State Observer Based Trajectory Linearization Control for Hypersonic Reentry Vehicle under High Maneuver Flight with Multiple Disturbances
    Zhang, Huiping
    Yu, Yue
    Wang, Honglun
    Liu, Yiheng
    2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2018,
  • [40] Based on minimum fuel consumption mode integrated optimal control of fixed-wing UAV flight propulsion system
    Li, Yong
    Han, Feifei
    Zhang, Xinzhe
    Peng, Kai
    Dang, Li
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2021, 93 (07): : 1133 - 1144