Analysis of optimal initial glide conditions for hypersonic glide vehicles

被引：0
|
作者：
机构：
[1] [1,Yan, Xiaodong
[2] Lyu, Shi
[3] 1,Tang, Shuo
来源：
Yan, X. (yan804@nwpu.edu.cn) | 1600年 / Chinese Journal of Aeronautics卷 / 27期
关键词：
Hypersonic glide vehicles (HGVs) are launched by a solid booster and glide through the atmosphere at high speeds. HGVs will be important means for rapid long-range delivery in the future. Given that the glide is unpowered; the initial glide conditions (IGCs) are crucial for flight. This paper aims to find the optimal IGCs to improve the maneuverability and decrease the constraints of HGVs. By considering the IGCs as experiment factors; we design an orthogonal table with three factors that have five levels each by using the orthogonal experimental design method. Thereafter; we apply the Gauss pseudospectral method to perform glide trajectory optimization by using each test of the orthogonal table as the initial condition. Based on the analytic hierarchy process; an integrated indicator is established to evaluate the IGCs; which synthesizes the indexes of the maneuverability and constraints. The integrated indicator is calculated from the trajectory optimization results. Finally; optimal IGCs and valuable conclusions are obtained by using range analysis; variance analysis; and regression analysis on the integrated indicator. © 2014 Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
引用
收藏
相关论文
共 50 条
  • [31] Analysis on Influence of the Bank Angle of Hypersonic Glide Vehicle
    Meng F.-Q.
    Tian K.-S.
    [J]. Tian, Kang-Sheng (tiankangsheng@tom.com), 1600, China Spaceflight Society (41): : 419 - 428
  • [32] Singular perturbation analysis of optimal glide
    Shapira, A
    Ben-Asher, JZ
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (05) : 915 - 918
  • [33] Robust Optimal Guidance for Hypersonic Glide Vehicle with Hinge Moment Constraint
    Cai Wei-wei
    Yang Le-ping
    Liu Xin-jian
    Zhu Yan-wei
    [J]. 2013 25TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2013, : 544 - 549
  • [34] Trajectory Tracking for Hypersonic Glide Vehicles Based on Improved Sine-AIMM
    Feng, Shan
    Tan, Qingke
    Li, Qingdong
    Ren, Zhang
    [J]. PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 5475 - 5480
  • [35] Analytic Time Reentry Cooperative Guidance for Multi-Hypersonic Glide Vehicles
    Xu, Hui
    Cai, Guangbin
    Fan, Yonghua
    Wei, Hao
    Li, Xin
    Wang, Yongchao
    [J]. APPLIED SCIENCES-BASEL, 2023, 13 (08):
  • [36] Asymmetric arms control and strategic stability: Scenarios for limiting hypersonic glide vehicles
    Williams, Heather
    [J]. JOURNAL OF STRATEGIC STUDIES, 2019, 42 (06) : 789 - 813
  • [37] Hypersonic Boost-Glide Weapons
    Acton, James M.
    [J]. SCIENCE & GLOBAL SECURITY, 2015, 23 (03) : 191 - 219
  • [38] Free Form Deformation Method Applied to Modeling and Design of Hypersonic Glide Vehicles
    Zhang, Bin
    Feng, Zhiwei
    Xu, Boting
    Yang, Tao
    [J]. IEEE ACCESS, 2019, 7 : 61400 - 61413
  • [39] Adaptive Higher Order Sliding Mode Attitude Control for Hypersonic Glide Vehicles
    Kong Weijie
    Yuan Hao
    Li Peng
    Zheng Zhiqiang
    [J]. PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 3436 - 3441
  • [40] Rapid Generation of Multi-Target Entry Trajectory for Hypersonic Glide Vehicles
    He RuiZhi
    Liu LuHua
    Tang GuoJian
    Bao WeiMin
    [J]. PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 5307 - 5312
12345