Title :
Dynamic Simulation of a Landing Gear System for Retraction and Deployment
Author :
Singh, Krishna Lok ; Upendranath, Vanam
Author_Institution :
Struct. Technol. Div., Nat. Aerosp. Labs. (NAL), Bangalore, India
Abstract :
In this article, dynamic simulation of landing gear system has been demonstrated. Brief introduction to the system modeling has been explained. Line Replaceable units have been modeled and simulated. The hydraulic power supply system has been explained in detail. The provision for leakage simulation has been demonstrated. The reduction in the pressure due to leakage has been presented. Finally the hydraulic component design components are explained for future demonstration of faults.
Keywords :
aerospace simulation; aircraft landing guidance; aircraft power systems; hydraulic systems; vehicle dynamics; hydraulic component design components; hydraulic power supply system; landing gear system dynamic simulation; leakage simulation; line replaceable units; retraction and deployment system; system modeling; Aircraft; Atmospheric modeling; Gears; Joints; Load modeling; Pistons; Pumps; Landing gear; dynamic; fault; system;
Conference_Titel :
Machine Intelligence and Research Advancement (ICMIRA), 2013 International Conference on
Conference_Location :
Katra
DOI :
10.1109/ICMIRA.2013.111
