@inproceedings{8e5b19f69fda43e79ec4fc4818a7c39e,
title = "Solution of aircraft trim problem based on genetic algorithms",
abstract = "It is important to solve aircraft equilibrium point for flight control law design and performance analyses. According to the characteristic of aircraft general straight flight, a solution to the aircraft trim problem was proposed by using genetic algorithms. First, the equilibrium equations were set up from aircraft six degree of freedom nonlinear equations. Then based on the equilibrium equations, the fitness functions were built by using dynamitic function, state variable, and output variable. And then the equilibrium equations were resolved by applying genetic algorithms. Finally, an example of trim algorithm was used with a simulation by an aircraft.",
keywords = "Equilibrium equations, Flight control, Genetic algorithms, Trim problem",
author = "Xiaoxiong Liu and Wu Yan and Sun Xun and Tang Qiang",
year = "2014",
doi = "10.1007/978-3-642-40630-0_4",
language = "英语",
isbn = "9783642406294",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Verlag",
number = "VOL. 2",
pages = "27--33",
booktitle = "Proceedings of the 9th International Symposium on Linear Drives for Industry Applications, LDIA 2013",
edition = "VOL. 2",
note = "9th International Symposium on Linear Drives for Industry Applications, LDIA 2013 ; Conference date: 07-07-2013 Through 10-07-2013",
}