Coupled Force and Moment Parameter Estimation for Aircraft
This paper presents the full application of the multipoint aerodynamic model for parameter estimation in high-angle-of-attack and high-angular-rate flight regimes. This model is intended for use in simulation and control design, and for the study of aerodynamic force distributions on the surfaces of...
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| Veröffentlicht in: | Journal of aircraft 1998-03, Vol.35 (2), p.247-253 |
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| container_end_page | 253 |
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| container_issue | 2 |
| container_start_page | 247 |
| container_title | Journal of aircraft |
| container_volume | 35 |
| creator | Cho, Yongseung Nagati, M. G |
| description | This paper presents the full application of the multipoint aerodynamic model for parameter estimation in high-angle-of-attack and high-angular-rate flight regimes. This model is intended for use in simulation and control design, and for the study of aerodynamic force distributions on the surfaces of an aircraft. The estimation technique used to illustrate the approach is simple regression with the equation error approach. |
| doi_str_mv | 10.2514/2.2291 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1998-03, Vol.35 (2), p.247-253 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_27480226 |
| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Aircraft Applied sciences Exact sciences and technology Ground, air and sea transportation, marine construction Miscellaneous transportation |
| title | Coupled Force and Moment Parameter Estimation for Aircraft |
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