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NLDI guidance control laws for close formation flight
This paper presents identification, control synthesis and simulation results for an YF-22 aircraft model designed, built, and instrumented at West Virginia University. The goal of the project was the experimental demonstration of formation flight for a set of 3 of the above models. In the planned fl...
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| container_end_page | 2977 vol. 4 |
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| creator | Campa, G. Seanor, B. Yu Gu Napolitano, M.R. |
| description | This paper presents identification, control synthesis and simulation results for an YF-22 aircraft model designed, built, and instrumented at West Virginia University. The goal of the project was the experimental demonstration of formation flight for a set of 3 of the above models. In the planned flight configuration, a pilot on the ground maintained controls of the leader aircraft while a follower aircraft was required to maintain a pre-defined position and orientation with respect to the leader. In this paper, the identification of both a linear model and a nonlinear model of the aircraft from (light data is shown first. Then, the control laws, that feature a linear inner loop controller and a NLDI (nonlinear dynamic inversion) based outer loop guidance controller, are discussed in detail. Finally, both simulation and flight test results are presented. |
| doi_str_mv | 10.1109/ACC.2005.1470426 |
| format | conference_proceeding |
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The goal of the project was the experimental demonstration of formation flight for a set of 3 of the above models. In the planned flight configuration, a pilot on the ground maintained controls of the leader aircraft while a follower aircraft was required to maintain a pre-defined position and orientation with respect to the leader. In this paper, the identification of both a linear model and a nonlinear model of the aircraft from (light data is shown first. Then, the control laws, that feature a linear inner loop controller and a NLDI (nonlinear dynamic inversion) based outer loop guidance controller, are discussed in detail. Finally, both simulation and flight test results are presented.</abstract><pub>IEEE</pub><doi>10.1109/ACC.2005.1470426</doi></addata></record> |
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| identifier | ISSN: 0743-1619 |
| ispartof | 2005 American Control Conference, 2005, p.2972-2977 vol. 4 |
| issn | 0743-1619 2378-5861 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_28969219 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Aerospace control Aerospace electronics Aerospace simulation Aerospace testing Aircraft Instruments Mechanical variables measurement Pressure measurement Q measurement Velocity measurement |
| title | NLDI guidance control laws for close formation flight |
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