Stability Margin Clearance of Missile Autopilot Using μ Anylysis
Stability Margin Clearance of Missile Autopilot Using μ Anylysis
- New search for: Hou, Zhen Qian
- New search for: Liang, Xiao Geng
- New search for: Wang, Wen Zheng
- New search for: Wang, Qiang Feng
A new method of stability margin clearance of missile autopilot is described. First, a model of linear fractional transformation form is established for missile has uncertain parameters; then, the system stability margin requirements are seen as a virtual uncertainty and introduced into the model; Finally, the model is analyzed, and the clearance results about the missile autopilot performance is obtained. The results show this is a more efficient and accurate clearance method than traditional ones.
Document information
Stability Margin Clearance of Missile Autopilot Using μ Anylysis
Applied Mechanics and Materials ; 198-199 ; 995-1000
2012-09-26
6 pages
Article (Journal)
Electronic Resource
English
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