RESULTS OF BEAVER AIRCRAFT PARAMETER IDENTIFICATION.

被引：0
作者：
Plaetschke, Ermin
Mulder, Jan Albert
Breeman, Jan Hendrik
机构：
来源：
Forschungsbericht - Deutsche Forschungs-und Versuchsanstalt fuer Luft-und Raumfahrt | 1983年
关键词：
AERODYNAMICS; -; Optimization;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A joint Dutch/German aircraft parameter identification program has been conducted to investigate various factors affecting identification results. Different design methods led to five test signals which were implemented via an electro-hydraulic control system in a flight test program with a De Havilland DHC-2 ″Beaver″ experimental aircraft. Aircraft parameters were calculated using two different parameter identification algorithms, classical maximum likelihood method and flight path reconstruction followed by linear regression analysis.
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