Title :
Simulation and analysis of the dynamic characteristics of the internally carried air-launched aircraft
Author :
Zheng Xiao-long ; Tang Shuo
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
Abstract :
To ensure the security of the entire air-launched carrier rockets system is an important issue in the research work. As the most expensive part of the system, the numerical simulation of the dynamic characteristics of the aircraft plays an important role. Dynamic equations of aircraft and its cargo during flight are derived in detail and dynamic models are established in accordance to the basic principles of theoretical mechanics and flight dynamics. The dynamic models are then utilized for the simulation of the process of the system. By comparing the simulation results and the real flight test measurements, the models are verified to be correct and precise. The dynamic characteristic of the aircraft under various conditions is also analyzed.
Keywords :
aerospace simulation; aircraft instrumentation; numerical analysis; rockets; aerospace simulation; air-launched aircraft; air-launched carrier rockets system; cargo; dynamic equations; flight dynamics; numerical simulation; security; Aerospace control; Aerospace simulation; Aircraft; Analytical models; Educational institutions; Numerical simulation; Robotics and automation; Rockets; Stability; Testing; air-launch; carrier rocket; dynamic characteristic; simulation;
Conference_Titel :
Informatics in Control, Automation and Robotics (CAR), 2010 2nd International Asia Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-5192-0
Electronic_ISBN :
1948-3414
DOI :
10.1109/CAR.2010.5456676