期刊名称：International Journal of Innovative Research in Science, Engineering and Technology
印刷版ISSN：2347-6710
电子版ISSN：2319-8753
出版年度：2015
卷号：4
期号：5
页码：3153
DOI：10.15680/IJIRSET.2015.0405094
出版社：S&S Publications
摘要：The project deals with the analysis of the aircraft stability. It determines the stability characteristics onthe basis of time and frequency domain using Bode plots and root locus plots. Aircrafts adopts an eclectic approach forparameter identification method. Time- domain method for stability control parameters estimation is used alongsidefrequency –domain methods which are chiefly used for determining flying qualities parameters. Stability is animportant factor for an aircraft and it is important for one should know about various stability factors beforecommenting on the aircraft stability. Determining the stability of the aircraft using complex mathematical calculationsis often time taking and approximate values are considered. In this project, the stability of aircrafts like – Boeing 767aircraft is analyzed. The stability factors are determined by using both complex mathematical calculations and usingsoftware- MATLAB. Using the software for determining the stability makes the work simple and it is less timeconsuming. It gives more accurate values and the results are more convincing.
关键词：Aircraft Stability; State Space Equation; Transfer Function; MATLAB.
