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Design of linear parameter‐varying controller for morphing aircraft using inexact scheduling parameters
by
Mu, Chaoxu
, Yang, Qian
, Cai, Guangbin
, Li, Xin
in
Aircraft
/ Aircraft control
/ Aircraft performance
/ Altitude
/ Control systems design
/ Controllers
/ Deformation
/ Design
/ Design parameters
/ Flight control systems
/ gain‐scheduling
/ inexact scheduling parameter
/ L2 gain
/ Linear matrix inequalities
/ linear parameter‐varying systems
/ Linear transformations
/ Morphing aircraft
/ Parameter robustness
/ Parameter uncertainty
/ Process parameters
/ Robust control
/ Scheduling
/ wing transition
2023
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Design of linear parameter‐varying controller for morphing aircraft using inexact scheduling parameters
by
Mu, Chaoxu
, Yang, Qian
, Cai, Guangbin
, Li, Xin
in
Aircraft
/ Aircraft control
/ Aircraft performance
/ Altitude
/ Control systems design
/ Controllers
/ Deformation
/ Design
/ Design parameters
/ Flight control systems
/ gain‐scheduling
/ inexact scheduling parameter
/ L2 gain
/ Linear matrix inequalities
/ linear parameter‐varying systems
/ Linear transformations
/ Morphing aircraft
/ Parameter robustness
/ Parameter uncertainty
/ Process parameters
/ Robust control
/ Scheduling
/ wing transition
2023
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Do you wish to request the book?
Design of linear parameter‐varying controller for morphing aircraft using inexact scheduling parameters
by
Mu, Chaoxu
, Yang, Qian
, Cai, Guangbin
, Li, Xin
in
Aircraft
/ Aircraft control
/ Aircraft performance
/ Altitude
/ Control systems design
/ Controllers
/ Deformation
/ Design
/ Design parameters
/ Flight control systems
/ gain‐scheduling
/ inexact scheduling parameter
/ L2 gain
/ Linear matrix inequalities
/ linear parameter‐varying systems
/ Linear transformations
/ Morphing aircraft
/ Parameter robustness
/ Parameter uncertainty
/ Process parameters
/ Robust control
/ Scheduling
/ wing transition
2023
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Design of linear parameter‐varying controller for morphing aircraft using inexact scheduling parameters
Journal Article
Design of linear parameter‐varying controller for morphing aircraft using inexact scheduling parameters
2023
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Overview
In this paper, the design problem of Gain‐Scheduled Output‐Feedback (GSOF) controllers using inexact scheduling parameters for morphing aircraft during the wing transition process is addressed. Both the stability of the closed‐loop system and the L2 gain performance can be guaranteed under the controller based on measured (not actual) scheduling parameters. Firstly, the linear parameter‐varying (LPV) model of morphing aircraft is established by Jacobian linearization and the additive uncertainty is introduced into the scheduling parameters. By employing non‐linear transformations, the problem is formulated as the solution to a set of parameter‐dependent linear matrix inequalities (LMI) with a single‐line search parameter. Finally, the robustness of the flight control system to the wing transition process is verified under the condition of both the uncertainty of aerodynamic parameters and of scheduling parameters.
Publisher
John Wiley & Sons, Inc,Wiley
Subject
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