|Table of Contents|

Control allocation optimization for missile with rudder fault(PDF)

《南京理工大学学报》（自然科学版）[ISSN:1005-9830/CN:32-1397/N]

Issue:
2017年05期
Page:
562-
Research Field:
Publishing date:

Info

Title:
Control allocation optimization for missile with rudder fault
Author(s):
Bao Zhenzhou1; Chen Jieqing1; Sun Ruisheng1; Zhu Gang2
1.School of Energy and Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,China; 2.Institute of Structural Mechanics,China Academy of Engineering Physics,Mianyang 621900,China
Keywords:
control allocation;  bases sequence approach;  rudder fault;  optimization design
PACS:
TP273
DOI:
10.14177/j.cnki.32-1397n.2017.41.05.004
Abstract:
The control allocation optimization of the missile with multi-control effectors under the rudder fault condition is researched and the optimization model is established.A bases-choose method based on the bases sequence control allocation is given to overcome the mutation problem due to the same effectiveness of many bases.The comparation with the traditional allocation shows that the method in this paper has the good performance of accuracy and rapidity,and it can provide the foundation of the fault-tolerant control of missiles.

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Last Update: 2017-09-30