DocumentCode
691146
Title
Modeling and Simulation to Improve Precision of Navigation for Space Aircraft Based on Time Compensation
Author
Zhang Jun ; Dong Wenjie ; Lin Jinyong ; Gao Xiaoying ; Yang Hu ; Li Shuangxi
Author_Institution
Nat. Key Lab. of Sci. & Technol. on Aerosp. Intell. Control, Beijing Aerosp. Autom. Control Inst., Beijing, China
fYear
2013
fDate
21-23 Sept. 2013
Firstpage
980
Lastpage
984
Abstract
In pervasive computing, the computer is no longer a single computing device, but an information device with the embedded processor, memory, communication module and various sensors together. This paper puts forward an algorithm to improve precision of navigation for space aircraft based on time compensation. The algorithm involves two-body movement time to correct the oblateness perturbation flying time, and then, improve the precision of navigation. On this basis, taking the advantage of pervasive computing in space aircraft application field, we involve pervasive computing technology into oblateness perturbation correction calculation. It provides the guarantee to precision of navigation for space aircraft, and enhances the auto-adaptability of space aircraft in complex space environment.
Keywords
aircraft computers; aircraft navigation; compensation; perturbation techniques; ubiquitous computing; complex space environment; information device; navigation precision; oblateness perturbation correction calculation; oblateness perturbation flying time; pervasive computing technology; space aircraft auto-adaptability; time compensation; two-body movement time; Aerospace control; Aerospace electronics; Aircraft; Aircraft navigation; Atmospheric modeling; Earth; Space vehicles; flying control computer; modeling and simulation; oblateness perturbation; pervasive computing;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2013 Third International Conference on
Conference_Location
Shenyang
Type
conf
DOI
10.1109/IMCCC.2013.218
Filename
6840608
Link To Document