DocumentCode
550306
Title
Constant bearing guidance for autonomous rendezvous
Author
Shen Yu-Heng ; Hou Ming-Shan
Author_Institution
Autom. Coll., Northwestern Polytech. Univ., Xi´an, China
fYear
2011
fDate
22-24 July 2011
Firstpage
342
Lastpage
346
Abstract
A constant bearing guidance law for autonomous rendezvous is proposed in this paper based on a line-of-sight(LOS) relative dynamic model with time-varying nonlinear and uncertainty. The LOS model is classified as a lateral model and a longitudinal model at first. Then the corresponding guidance law and related parameters selection for the two models are discussed based on sliding model control and Lyapunov stability theory. The parallel proximity is achieved with the lateral guidance meanwhile the rendezvous range and velocity requirements are satisfied with the longitudinal guidance. Numerical simulation shows that the time-varying nonlinear and uncertainty can be overcame with the designed guidance strategy just by using the autonomous navigation information.
Keywords
Lyapunov methods; aircraft landing guidance; nonlinear control systems; time-varying systems; variable structure systems; velocity control; LOS relative dynamic model; Lyapunov stability theory; autonomous navigation information; autonomous rendezvous; constant bearing guidance law; designed guidance strategy; lateral guidance; lateral model; line-of-sight relative dynamic model; longitudinal guidance; longitudinal model; parallel proximity; parameters selection; rendezvous range; sliding model control; time-varying nonlinear system; uncertainty; velocity requirements; Electronic mail; Navigation; Numerical models; Numerical simulation; Satellites; Space vehicles; Uncertainty; Autonomous Rendezvous; Constant Bearing; Guidance; Nonlinear; Variable Structure;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2011 30th Chinese
Conference_Location
Yantai
ISSN
1934-1768
Print_ISBN
978-1-4577-0677-6
Electronic_ISBN
1934-1768
Type
conf
Filename
6000644
Link To Document