Generation of Landing Footprints for Re-entry Vehicles Based on Lateral Profile Priority

被引:0
|
作者
Yuan-long Zhang
Yu Xie
Xin Xu
机构
[1] National University of Defense Technology,
关键词
Re-entry vehicles; Landing footprints; Three-dimensional acceleration profile; Trajectory generation;
D O I
暂无
中图分类号
学科分类号
摘要
This study proposes a method for calculating the landing footprints of re-entry vehicles based on the three-dimensional acceleration profile. Unlike the traditional case in which the reference angle-of-attack profile is given in advance, here, the manoeuvrability of the vehicle is enhanced owing to the release of the constraints of the angle-of-attack profile. Compared with the traditional methods of generating landing footprints, this method is more challenging because it is necessary to adjust the angle-of-attack and the bank angle simultaneously to obtain all feasible trajectories. With the enhancement of manoeuvrability, the traditional landing footprints solving strategy with a fixed bank direction under the premise of a given angle-of-attack is expected to make the footprints of the result locally smaller. Therefore, a layered design based on a three-dimensional profile and lateral priority strategy is proposed to solve the problem. First, a lateral flight corridor considering various path constraints is constructed. Then, the boundary interpolation of the flight corridor is used to generate an initial lateral profile. The longitudinal profile corresponding to the lateral profile is analysed according to the coupling relationship between the longitudinal and lateral profiles, and the corresponding trajectory is then obtained by numerical integration. The tentative landing footprints can be obtained by traversing all feasible profiles in the lateral corridor. Finally, to solve the problem of inaccuracy in the solution of landing footprints, the core innovation of this study is the generation of multiple groups of different lateral flight corridors by adjusting the initial and terminal bank directions. By solving the tentative landing footprints under different flight corridors and merging them, highly accurate landing footprints were obtained. The proposed method is tested with the CAV-H model of Lockheed Martin, and the results are compared with those of traditional methods to verify its effectiveness and feasibility.
引用
收藏
页码:261 / 273
页数:12
相关论文
共 50 条
  • [1] Generation of Landing Footprints for Re-entry Vehicles Based on Lateral Profile Priority
    Zhang, Yuan-long
    Xie, Yu
    Xu, Xin
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2023, 24 (01) : 261 - 273
  • [2] Precise re-entry and landing of propellantless spacecraft
    Fedele, Alberto
    Omar, Sanny
    Cantoni, Stefania
    Savino, Raffaele
    Bevilacqua, Riccardo
    ADVANCES IN SPACE RESEARCH, 2021, 68 (11) : 4336 - 4358
  • [3] An optimization-based procedure for self-generation of Re-entry Vehicles shape
    Viviani, Antonio
    Iuspa, Luigi
    Aprovitola, Andrea
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 68 : 123 - 134
  • [4] Rapid Generation of Accurate Entry Landing Footprints
    Lu, Ping
    Xue, Songbai
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (03) : 756 - 767
  • [5] Aerodynamics of ducted re-entry vehicles
    CANBU SERENE RAJ
    MNARASIMHAVARADHAN
    NVAISHNAVI
    SARUNVINTHAN
    AAL ARJANI
    SNADARAJA PILLAI
    Chinese Journal of Aeronautics, 2020, 33 (07) : 1837 - 1849
  • [6] Aerodynamics of ducted re-entry vehicles
    Raj, C. Anbu Serene
    Narasimhavaradhan, M.
    Vaishnavi, N.
    Arunvinthan, S.
    Al Arjani, A.
    Pillai, S. Nadaraja
    CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (07) : 1837 - 1849
  • [7] Aerodynamics of ducted re-entry vehicles
    C.ANBU SERENE RAJ
    M.NARASIMHAVARADHAN
    N.VAISHNAVI
    S.ARUNVINTHAN
    A.AL ARJANI
    S.NADARAJA PILLAI
    Chinese Journal of Aeronautics , 2020, (07) : 1837 - 1849
  • [8] THERMIONIC GENERATOR FOR RE-ENTRY VEHICLES
    LEBLANC, AR
    GRANNEMANN, WW
    PROCEEDINGS OF THE IEEE, 1964, 52 (11) : 1302 - &
  • [9] Selective lateral re-entry system
    Anon
    JPT, Journal of Petroleum Technology, 2000, 52 (06):
  • [10] Selective lateral re-entry system
    不详
    JOURNAL OF PETROLEUM TECHNOLOGY, 2000, 52 (06): : 56 - +