Methodology of clearance of flight control law

Xi Zhou; Lin Liu; Zongji Chen; Weiqi Li

Methodology of clearance of flight control law

Xi Zhou^*
, Lin Liu
, Zongji Chen
, Weiqi Li

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

Research output: Contribution to conference › Paper › peer-review

Abstract

This paper analysis the methodology of flight clearance and presents an example to verify the correctness and feasibility of the methods used in flight clearance process. The main goal of flight clearance is to try structured singular value (μ) analysis on the flight control system when some parameters in the system vary in a certain range. As μ- analysis can only be done on a linear fractional transformation (LFT) model, the first step of flight clearance is to generate the LFT model of the flight control system. An X-Fighter is chosen to realize the methods proposed in this paper. Simulation results demonstrate that X-Fighter passes the flight clearance. It not only proves the robustness of the control law but also confirms the correctness and feasibility of the methods used in the flight control process.

Original language	English
Pages	258-262
Number of pages	5
State	Published - 2005
Event	Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005 - Beijing, China Duration: 24 Oct 2005 → 27 Oct 2005

Conference

Conference	Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005
Country/Territory	China
City	Beijing
Period	24/10/05 → 27/10/05

Keywords

Flight clearance
LFT
Robust stability
Uncertain parameter
μ-analysis

Cite this

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title = "Methodology of clearance of flight control law",

abstract = "This paper analysis the methodology of flight clearance and presents an example to verify the correctness and feasibility of the methods used in flight clearance process. The main goal of flight clearance is to try structured singular value (μ) analysis on the flight control system when some parameters in the system vary in a certain range. As μ- analysis can only be done on a linear fractional transformation (LFT) model, the first step of flight clearance is to generate the LFT model of the flight control system. An X-Fighter is chosen to realize the methods proposed in this paper. Simulation results demonstrate that X-Fighter passes the flight clearance. It not only proves the robustness of the control law but also confirms the correctness and feasibility of the methods used in the flight control process.",

keywords = "Flight clearance, LFT, Robust stability, Uncertain parameter, μ-analysis",

author = "Xi Zhou and Lin Liu and Zongji Chen and Weiqi Li",

year = "2005",

language = "英语",

pages = "258--262",

note = "Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005 ; Conference date: 24-10-2005 Through 27-10-2005",

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TY - CONF

T1 - Methodology of clearance of flight control law

AU - Zhou, Xi

AU - Liu, Lin

AU - Chen, Zongji

AU - Li, Weiqi

PY - 2005

Y1 - 2005

N2 - This paper analysis the methodology of flight clearance and presents an example to verify the correctness and feasibility of the methods used in flight clearance process. The main goal of flight clearance is to try structured singular value (μ) analysis on the flight control system when some parameters in the system vary in a certain range. As μ- analysis can only be done on a linear fractional transformation (LFT) model, the first step of flight clearance is to generate the LFT model of the flight control system. An X-Fighter is chosen to realize the methods proposed in this paper. Simulation results demonstrate that X-Fighter passes the flight clearance. It not only proves the robustness of the control law but also confirms the correctness and feasibility of the methods used in the flight control process.

AB - This paper analysis the methodology of flight clearance and presents an example to verify the correctness and feasibility of the methods used in flight clearance process. The main goal of flight clearance is to try structured singular value (μ) analysis on the flight control system when some parameters in the system vary in a certain range. As μ- analysis can only be done on a linear fractional transformation (LFT) model, the first step of flight clearance is to generate the LFT model of the flight control system. An X-Fighter is chosen to realize the methods proposed in this paper. Simulation results demonstrate that X-Fighter passes the flight clearance. It not only proves the robustness of the control law but also confirms the correctness and feasibility of the methods used in the flight control process.

KW - Flight clearance

KW - LFT

KW - Robust stability

KW - Uncertain parameter

KW - μ-analysis

UR - https://www.scopus.com/pages/publications/84902499688

M3 - 论文

AN - SCOPUS:84902499688

SP - 258

EP - 262

T2 - Asian Simulation Conference 2005, ASC 2005 and the 6th International Conference on System Simulation and Scientific Computing, ICSC 2005

Y2 - 24 October 2005 through 27 October 2005

ER -

Methodology of clearance of flight control law

Abstract

Conference

Keywords

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