DocumentCode :
690368
Title :
Research on Climb Performance and 4D Trajectory Prediction of Aircraft
Author :
Xiaoyan Zhang ; Yunxiang Han
Author_Institution :
Coll. of Air Traffic Manage., Civil Aviation Flight Univ. of China, Deyang, China
fYear :
2013
fDate :
14-15 Dec. 2013
Firstpage :
390
Lastpage :
393
Abstract :
4D reckoning is a core technology to the next generation of air transport management. This paper mainly do research on the aircraft dynamics model under a given flight profile of different phases of flight performance and aircraft performance differences. Then, proposed two models: state switching transition model between different phases of flight, System evolution model under the continuous variation states that aircraft weight, indicated airspeed, altitude, distance and others. Using the mode of hybrid system recursive simulation obtained 4D trajectory of aircraft and analyzed the effects of various factors on the performance of the aircraft´s climb.
Keywords :
aircraft; recursive estimation; vehicle dynamics; air transport management; aircraft 4D trajectory prediction; aircraft altitude; aircraft climb performance; aircraft distance; aircraft dynamics model; aircraft indicated airspeed; aircraft weight; continuous variation states; flight performance; flight profile; hybrid system recursive simulation; state switching transition model; system evolution model; Air traffic control; Aircraft; Atmospheric modeling; Educational institutions; Fuels; Mathematical model; Trajectory; 4D trajectory; a new generation of air traffic control automation system; climb performance; hybrid system model;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Sciences and Applications (CSA), 2013 International Conference on
Conference_Location :
Wuhan
Type :
conf
DOI :
10.1109/CSA.2013.98
Filename :
6835625
Link To Document :
بازگشت