Title : 
Research on response characteristic of moving-mass controlled flying vehicle
         
        
            Author : 
Shenghong Xu ; Wenjing Cao ; Ruitao Li
         
        
            Author_Institution : 
Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
         
        
        
        
        
        
            Abstract : 
The response characteristics of the moving-mass controlled flying vehicle is researched based on the moving-mass control system model of the flying saucer. Simulation results show that when the vehicle flies in the thick atmosphere at low altitude, the states of the vehicle are disturbed by the movement of the sliding mass block, but the disturbance does not appear when the vehicle flies at superhigh altitude or in the outer space. The cause of the difference is analyzed, and the influencing factors of the disturbance are studied with simulation.
         
        
            Keywords : 
aircraft control; flying saucer; moving-mass control system model; moving-mass controlled flying vehicle; sliding mass block; vehicle response characteristics; Aerodynamics; Aerospace electronics; Control systems; Equations; Force; Mathematical model; Vehicles;
         
        
        
        
            Conference_Titel : 
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
         
        
            Conference_Location : 
Yantai
         
        
            Print_ISBN : 
978-1-4799-4700-3
         
        
        
            DOI : 
10.1109/CGNCC.2014.7007509