Volume 16 Issue 2
Apr.  2001
Turn off MathJax
Article Contents
HE Li ming, FAN Ding. Application of SQP to Multi-Object Optimization of Turbofan Engine Acceleration Control[J]. Journal of Aerospace Power, 2001, 16(2): 179-181,178.
Citation: HE Li ming, FAN Ding. Application of SQP to Multi-Object Optimization of Turbofan Engine Acceleration Control[J]. Journal of Aerospace Power, 2001, 16(2): 179-181,178.

Application of SQP to Multi-Object Optimization of Turbofan Engine Acceleration Control

  • Received Date: 2000-06-13
  • Rev Recd Date: 2000-09-25
  • Publish Date: 2001-04-28
  • The control of aircraft engine acceleration is the focus in the field of aeroengine control.Sequential Quadratic Programming(SQP)based on nonlinear programming is used to control turbofan engine acceleration.Meanwhile the Linear Weighted Sum of multi object optimization has been introduced to attain double variable control in turbofan engine acceleration process.In the study every constraint of the acceleration process has been thoroughly considered.The simulation results show that the application of multi object optimization to turbofan engine acceleration control is feasible.It can bring the engine potentialities into full play and improve the acceleration performance significantly.

     

  • loading
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1643) PDF downloads(447) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return