The control of a parallel hybrid-electric propulsion system for a small unmanned aerial vehicle using a CMAC neural network

被引:50
作者
Harmon, FG [1 ]
Frank, AA [1 ]
Joshi, SS [1 ]
机构
[1] Univ Calif Davis, Dept Mech & Aeronaut Engn, Davis, CA 95616 USA
关键词
D O I
10.1016/j.neunet.2005.06.030
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
A Simulink model, a propulsion energy optimization algorithm, and a CMAC controller were developed for a small parallel hybrid-electric unmanned aerial vehicle (UAV). The hybrid-electric UAV is intended for military, homeland security, and disaster-monitoring missions involving intelligence, surveillance, and reconnaissance (ISR). The Simulink model is a forward-facing simulation program used to test different control strategies. The flexible energy optimization algorithm for the propulsion system allows relative importance to be assigned between the use of gasoline, electricity, and recharging. A cerebellar model arithmetic computer (CMAC) neural network approximates the energy optimization results and is used to control the parallel hybrid-electric propulsion system. The hybrid-electric UAV with the CMAC controller uses 67.3% less energy than a two-stroke gasoline-powered UAV during a 1-h ISR mission and 37.8% less energy during a longer 3-h ISR mission. Published by Elsevier Ltd.
引用
收藏
页码:772 / 780
页数:9
相关论文
共 19 条
[1]  
ALBUS JS, 1975, J DYNAMIC SYSTEMS ME, V63, P228
[2]  
ALDRIDGE EC, 2003, UNMANNED AERIAL VEHI
[3]  
[Anonymous], P INT JOINT C NEUR N
[4]  
[Anonymous], J DYN SYST MEAS CONT, DOI DOI 10.1115/1.3426922
[5]  
[Anonymous], 1985, INTRO FLIGHT
[6]  
BROOKER A, 2002, ADVISOR DOCUMENTATIO
[7]  
Brown M, 1994, NEUROFUZZY ADAPTIVE
[8]  
FRANCISCO AB, 2002, THESIS U CALIFORNIA
[9]  
FRANK AA, 2000, CONTROL METHOD APPAR
[10]  
GLANZ FH, 1991, IEEE C NEURAL NETWOR