Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation
The aim of “Robustness Analysis” is to assess aircraft stability in the presence of all admissible uncertainties. Models that are able to describe the aircraft dynamics by taking into account all uncertainties over a region inside the flight envelope have therefore been developed, using Linear Fract...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2017-12-01
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| Series: | INCAS Bulletin |
| Subjects: | |
| Online Access: | http://bulletin.incas.ro/files/boughari__botez__theel__ghazi__vol_9_iss_4__part_1.pdf |
| _version_ | 1811238908771434496 |
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| author | Yamina BOUGHARI Ruxandra Mihaela BOTEZ Florian THEEL Georges GHAZI |
| author_facet | Yamina BOUGHARI Ruxandra Mihaela BOTEZ Florian THEEL Georges GHAZI |
| author_sort | Yamina BOUGHARI |
| collection | DOAJ |
| description | The aim of “Robustness Analysis” is to assess aircraft stability in the presence of all admissible uncertainties. Models that are able to describe the aircraft dynamics by taking into account all uncertainties over a region inside the flight envelope have therefore been developed, using Linear Fractional Representation (LFR). In this paper Part 1 a friendly Graphical User Interface is developed to facilitate the generation of Linear Fractional Representation uncertainty models for the Cessna Citation X aircraft using 12 weight and Xcg configurations; thus, 26 regions of the flight envelope are developed for different Weight/ Xcg configurations to study the aircraft’s longitudinal motion. In the aim to analyzed the robustness stability of Cessna Citation X in Part 2 using the Graphical User Interface developed in the Clearance Of Flight Control Laws Using Optimization (COFCLUO) project. This project aimed to boost the aircraft safety using computer computation. |
| first_indexed | 2024-04-12T12:50:32Z |
| format | Article |
| id | doaj.art-5ca38ae4b96e412ca0f038890a1f79a0 |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-04-12T12:50:32Z |
| publishDate | 2017-12-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-5ca38ae4b96e412ca0f038890a1f79a02022-12-22T03:32:29ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282017-12-0194314310.13111/2066-8201.2017.9.4.4Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs GenerationYamina BOUGHARI0Ruxandra Mihaela BOTEZ1Florian THEEL2Georges GHAZI3ETS, Laboratory of Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre Dame West, Montreal, Que., Canada, H3C-1K3, yamina.boughari.1@ens.etsmtl.caETS, Laboratory of Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre Dame West, Montreal, Que., Canada, H3C-1K3, Ruxandra.Botez@etsmtl.ca*ETS, Laboratory of Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre Dame West, Montreal, Que., Canada, H3C-1K3, f.theel@gmail.comETS, Laboratory of Active Controls, Avionics and AeroServoElasticity LARCASE, 1100 Notre Dame West, Montreal, Que., Canada, H3C-1K3, georges.ghazi.1@ens.etsmtl.caThe aim of “Robustness Analysis” is to assess aircraft stability in the presence of all admissible uncertainties. Models that are able to describe the aircraft dynamics by taking into account all uncertainties over a region inside the flight envelope have therefore been developed, using Linear Fractional Representation (LFR). In this paper Part 1 a friendly Graphical User Interface is developed to facilitate the generation of Linear Fractional Representation uncertainty models for the Cessna Citation X aircraft using 12 weight and Xcg configurations; thus, 26 regions of the flight envelope are developed for different Weight/ Xcg configurations to study the aircraft’s longitudinal motion. In the aim to analyzed the robustness stability of Cessna Citation X in Part 2 using the Graphical User Interface developed in the Clearance Of Flight Control Laws Using Optimization (COFCLUO) project. This project aimed to boost the aircraft safety using computer computation.http://bulletin.incas.ro/files/boughari__botez__theel__ghazi__vol_9_iss_4__part_1.pdfLinear Fractional RepresentationFlight Control ClearanceStability Analysis Robustness Analysis |
| spellingShingle | Yamina BOUGHARI Ruxandra Mihaela BOTEZ Florian THEEL Georges GHAZI Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation INCAS Bulletin Linear Fractional Representation Flight Control Clearance Stability Analysis Robustness Analysis |
| title | Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation |
| title_full | Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation |
| title_fullStr | Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation |
| title_full_unstemmed | Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation |
| title_short | Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation |
| title_sort | cessna citation x business aircraft eigenvalue stability part 1 a new gui for the lfrs generation |
| topic | Linear Fractional Representation Flight Control Clearance Stability Analysis Robustness Analysis |
| url | http://bulletin.incas.ro/files/boughari__botez__theel__ghazi__vol_9_iss_4__part_1.pdf |
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