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|a 9789176854501
|q (electronic bk.)
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|a MiAaPQ
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|c MiAaPQ
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|a Simon, Daniel.
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|a Fighter Aircraft Maneuver Limiting Using MPC :
|b Theory and Application.
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|a 1st ed.
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|a Linköping :
|b Linkopings Universitet,
|c 2017.
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|c {copy}2017.
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|a 1 online resource (202 pages)
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a Linköping Studies in Science and Technology. Dissertations Series ;
|v v.1881
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|a Intro -- Abstract -- Populärvetenskaplig sammanfattning -- Acknowledgments -- Contents -- Notation -- 1 Introduction -- 1.1 Background and research motivation -- 1.2 Previous research -- 1.3 Publications and main contributions -- 1.4 Thesis outline -- I Theory -- 2 Background on optimization and polytopic geometry -- 2.1 Optimization -- 2.1.1 Convex optimization -- 2.1.2 Duality -- 2.1.3 Nonconvex optimization -- 2.1.4 Mixed integer optimization -- 2.2 Convex polytopic geometry -- 3 Aircraft flight dynamics and flight control design -- 3.1 The nonlinear dynamics -- 3.2 The linearized dynamics -- 3.3 Fighter aircraft flight control law design -- 3.4 The ARES and ADMIRE models -- 3.4.1 ARES baseline LQ controller -- 4 Introduction to model predictive control -- 4.1 Introduction -- 4.2 Linear MPC -- 4.2.1 Stability -- 4.2.2 Reference tracking -- 4.2.3 Integral control -- 4.2.4 Slack variables -- 4.2.5 The explicit solution -- 4.3 Nonlinear MPC -- 5 A low complexity reference tracking MPC algorithm -- 5.2 The proposed controller -- 5.2.1 Vertex enumeration reformulation -- 5.2.2 Dual formulation of terminal set constraints -- 5.2.3 The QP formulation -- 5.2.4 Stability and feasibility of the proposed algorithm -- 5.3 Examples from the aeronautical industry -- 5.3.1 Maneuver limitations on a fighter aircraft -- 5.3.2 Nonlinear aircraft performance -- 5.3.3 Helicopter flight envelope protection -- 6 Method for guaranteed stability and recursive feasibility in nonlinear MPC -- 6.1 Introduction -- 6.1.1 Feedback linearization -- 6.2 The proposed algorithm -- 6.2.1 Nonlinear constraint approximations -- 6.2.2 MPC receding horizon setup -- 6.3 Examples -- 7 Testing stability and robustness of MPC controllers -- 7.1 Introduction -- 7.2 The MILP stability test -- 7.2.1 Exploiting structure in the MILP -- 7.2.2 A sufficient but not necessary condition.
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|a 7.2.3 Computational complexity of the stability test -- 7.2.4 Move blocking and no stabilizing constraints -- 7.3 Testing for robust stability -- 7.3.2 The robust stability condition -- 7.3.3 Reformulation into a MILP -- 7.3.4 Robust stability of an agile fighter aircraft -- II Application -- 8 Industrial implementation of an MPC controller for a fighter aircraft -- 8.1 Introduction -- 8.2 The MPC controller structure -- 8.3 Tuning of the MPC controller -- 8.4 Simulator testing -- 9 Aircraft maneuver limiting using command governors -- 9.1 Introduction -- 9.2 Reference and command governors -- 9.3 Command governor design -- 9.3.1 N-step prediction approach -- 9.3.2 Selection of discretization technique -- 9.3.3 Model error correction term -- 9.3.4 Selection of objective function and parameterization of the reference -- 9.4 Simulation results -- 10 Conclusions and future work -- Bibliography.
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|a Description based on publisher supplied metadata and other sources.
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| 590 |
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|a Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
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|a Electronic books.
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|i Print version:
|a Simon, Daniel
|t Fighter Aircraft Maneuver Limiting Using MPC
|d Linköping : Linkopings Universitet,c2017
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| 797 |
2 |
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|a ProQuest (Firm)
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| 830 |
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|a Linköping Studies in Science and Technology. Dissertations Series
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| 856 |
4 |
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|u https://ebookcentral.proquest.com/lib/matrademy/detail.action?docID=5049580
|z Click to View
|
