Title :
UAV Simulator-Based Simulation of Flight Control System
Author :
Jin Guo-dong ; Gu Liang-xian ; Lu Li-bin
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an
Abstract :
Most UAV flight control system simulation was used for evaluating the quality of UAV and designing it, however, the results failed to conform to actual flight laws. According to the need of UAV simulator in actually, a new way which was convenient for engineering computing and appropriated for simulation training was built for simulating flight control system. With the actual flight figures, flight parameters were modified by least squares method curve fitting. The system offers a way for developing UAV simulation training system, thus of great value in both theory and practice.
Keywords :
aerospace control; computer based training; curve fitting; least squares approximations; remotely operated vehicles; UAV simulator-based simulation; curve fitting; engineering computing; flight control system; least squares method; simulation training; unmanned aerial vehicle; Aerospace control; Aerospace engineering; Aerospace simulation; Atmosphere; Atmospheric modeling; Computational modeling; Educational institutions; Engines; Mathematical model; Unmanned aerial vehicles;
Conference_Titel :
Intelligent Systems and Applications, 2009. ISA 2009. International Workshop on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-3893-8
Electronic_ISBN :
978-1-4244-3894-5
DOI :
10.1109/IWISA.2009.5073226
