Knowledge Network Node
Missiles and Space Vehicles. 2025, (01) Core

Modeling and Application Research on Vertical Recovery Control Capability of Launch VehiclesChinese Full TextEnglish Full Text (MT)

YI Xin;HU Haifeng;HE Yuanjun;Beijing Aerospace Automatic Control Institute;China Manned Space Engineering Office;

Abstract: When the design input is limited during the initial stage of scheme argumentation, in order to solve the problem of how to conduct control capability analysis quickly and effectively, the adaptability of traditional control capability analysis method is analyzed. A set of controllability analytical method for reentrant launch vehicles is researched by dynamic modeling and original method improving. And under the premise of limited control capability, the constraint conditions for allowable fligh... More
Keywords：

reentrant launch vehicles; controllability and analytic method; balance equation; flight condition constrains; dynamic modeling;

  • Series：

    (C) Architecture/ Energy/ Traffic/ Electromechanics, etc

  • Subject：

    Aeronautics and Astronautics Science and Engineering

  • Classification Code：

    V475.1;V448.1

Download the mobile appuse the app to scan this coderead the article.

Tips: Please download CAJViewer to view CAJ format full text.

Download: 77 Page: 73-77+106 Pagecount: 6 Size: 1052K

Related Literature
  • Similar Article
  • Reader Recommendation
  • Associated Author