| タイトル | System identification methods for aircraft flight control development and validation |
| 本文（外部サイト） | http://hdl.handle.net/2060/19960003220 |
| 著者（英） | Tischler, Mark B. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1995-10-01 |
| 言語 | eng |
| 内容記述 | System-identification methods compose a mathematical model, or series of models, from measurements of inputs and outputs of dynamic systems. The extracted models allow the characterization of the response of the overall aircraft or component subsystem behavior, such as actuators and on-board signal processing algorithms. This paper discusses the use of frequency-domain system-identification methods for the development and integration of aircraft flight-control systems. The extraction and analysis of models of varying complexity from nonparametric frequency-responses to transfer-functions and high-order state-space representations is illustrated using the Comprehensive Identification from FrEquency Responses (CIFER) system-identification facility. Results are presented for test data of numerous flight and simulation programs at the Ames Research Center including rotorcraft, fixed-wing aircraft, advanced short takeoff and vertical landing (ASTOVL), vertical/short takeoff and landing (V/STOL), tiltrotor aircraft, and rotor experiments in the wind tunnel. Excellent system characterization and dynamic response prediction is achieved for this wide class of systems. Examples illustrate the role of system-identification technology in providing an integrated flow of dynamic response data around the entire life-cycle of aircraft development from initial specifications, through simulation and bench testing, and into flight-test optimization. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 96N13229
NIPS-95-05604
NASA-TM-110369
NAS 1.15:110369
A-950097
USAATCOM-TR-95-A-007 |
| 権利 | No Copyright |
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