Title :
Study of Flying Control Computer Based on Plug-and-Play Method
Author :
Lin Jin-Yong ; Dong Wen-Jie ; Wang Yan-Ning ; Liu Jing-Jing ; Zhou Chun-Mei
Author_Institution :
Nat. Key Lab. of Sci. & Technol. on Aerosp. Intell. Control, Beijing Aerosp. Autom. Control Inst., Beijing, China
Abstract :
The applications of plug and play (PnP) method to flying control computer for aerospace launch vehicle is studied, and the plug-and-play model of flying control computer is discussed. Then the PnP design scheme of flying control computer is presented, also the validation experiment is carried through. At last, a simple demonstration system is built, and the research method is tested and analyzed, The test result shows that the above PnP design scheme is correct and will support the future aerospace launch vehicle for upholding the responsive ability.
Keywords :
aerospace control; aircraft; PnP method; aerospace launch vehicle; flying control computer; plug-and-play method; Aerospace control; Aerospace electronics; Computational modeling; Computers; Hardware; Runtime; Software; Plug-and-Play; aerospace launch vehicle; design scheme; flying control computer;
Conference_Titel :
Instrumentation and Measurement, Computer, Communication and Control (IMCCC), 2014 Fourth International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4799-6574-8
DOI :
10.1109/IMCCC.2014.48
