Title :
Suppression of aerodynamic coupled parasitic loop
Author :
Fugui Li;Hong Zhao
Author_Institution :
China Academy of Launch Vehicle Technology, Beijing, China
Abstract :
Aerodynamic coupled parasitic loop is introduced in this paper. The essence of AADP(Aileron alone departure parameter) and LCDP(Lateral control departure parameter) criterion was studied with this loop. The effect of aerodynamic coupled parasitic loop also was researched. The method to restrain the harmful effect of this loop is also present, and the AADP and LCDP criterion are amended for easy use. The study shows that with the amended criterion the aerodynamic configuration of the vehicle and the control parameters could be adjusted to reduce the harmful effect of the aerodynamic coupled parasitic loop.
Keywords :
"Aerodynamics","Vehicle dynamics","Mathematical model","Vehicles","Stability criteria","Control systems"
Conference_Titel :
Information and Automation, 2015 IEEE International Conference on
DOI :
10.1109/ICInfA.2015.7279497