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| Fältnamn | Indikatorer | Metadata |
|---|---|---|
| 000 | 02899naa a2200469 4500 | |
| 001 | oai:DiVA.org:liu-24076 | |
| 003 | SwePub | |
| 008 | 091007s2004 | |||||||||||000 ||eng| | |
| 024 | 7 | a https://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-240762 URI |
| 024 | 7 | a https://doi.org/10.2514/6.2004-48672 DOI |
| 040 | a (SwePub)liu | |
| 041 | a engb eng | |
| 042 | 9 SwePub | |
| 072 | 7 | a ref2 swepub-contenttype |
| 072 | 7 | a kon2 swepub-publicationtype |
| 100 | 1 | a Ståhl Gunnarsson, Karinu Saab AB, Sweden4 aut |
| 245 | 1 0 | a Clearance of Flight Control Laws using Linear Fractional Transformations |
| 264 | c 2004-06-22 | |
| 264 | 1 | a Reston, Virigina :b American Institute of Aeronautics and Astronautics,c 2004 |
| 338 | a print2 rdacarrier | |
| 520 | a The problem of flight clearance of linear stability requirements in the complete flight evelope is studied. The approach is to use mu-analysis of linear fractional transformations description of the system dynamics augmented with an uncertainty model of the clearance criteria. Two methods to derive the linear fractional transformations are used and compared: the Trends and Bands method and rational approximations. The two approaches are applied to a UAV demostrator model. The resulting models are analyzed by mu-sensitivites in order to demonstrate how this can be used to reduce the order of the linear fractional transformations description. A number of algorithms to compute upper and lower bounds on mu are also compared. Results from applying the clearance criteria to the UAV demonstrator model are given. | |
| 650 | 7 | a TEKNIK OCH TEKNOLOGIERx Elektroteknik och elektronikx Reglerteknik0 (SwePub)202022 hsv//swe |
| 650 | 7 | a ENGINEERING AND TECHNOLOGYx Electrical Engineering, Electronic Engineering, Information Engineeringx Control Engineering0 (SwePub)202022 hsv//eng |
| 653 | a Linear fractional tranformation | |
| 653 | a LFT | |
| 653 | a Structured singular value | |
| 653 | a SSV | |
| 653 | a Linear matrix inequality | |
| 653 | a LMI | |
| 653 | a Lyapunov function | |
| 653 | a Flight clearance | |
| 653 | a Stability margin | |
| 653 | a TECHNOLOGY | |
| 653 | a TEKNIKVETENSKAP | |
| 700 | 1 | a Hansson, Jörgenu Saab AB, Sweden4 aut |
| 700 | 1 | a Karlsson, Fredriku Saab AB, Sweden4 aut |
| 700 | 1 | a Hansson, Andersu Linköpings universitet,Reglerteknik,Tekniska högskolan4 aut0 (Swepub:liu)andha17 |
| 700 | 1 | a Wallin, Ragnar,d 1962-u Linköpings universitet,Reglerteknik,Tekniska högskolan4 aut0 (Swepub:liu)ragwa15 |
| 710 | 2 | a Saab AB, Swedenb Reglerteknik4 org |
| 773 | 0 | t Proceedings of the 2004 AIAA Guidance, Navigation and Control Conference and Exhibitd Reston, Virigina : American Institute of Aeronautics and Astronauticsz 9781624100734 |
| 856 | 4 8 | u https://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-24076 |
| 856 | 4 8 | u https://doi.org/10.2514/6.2004-4867 |
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