DocumentCode
2288514
Title
QoS tradeoffs for guidance, navigation, and control
Author
Ella, M. ; Sanner, Robert M.
Author_Institution
Dept. of Aerosp. Eng., Maryland Univ., College Park, MD, USA
Volume
7
fYear
2002
fDate
2002
Firstpage
523576
Abstract
Future space missions will require onboard autonomy to reduce data, plan activities, and react appropriately to complex dynamic events. Software to support such behaviors is computationally-intensive but must execute with sufficient speed to accomplish mission goals. The limited processing resources onboard spacecraft must be split between the new software and required guidance, navigation, control, and communication tasks. To-date, control-related processes have been scheduled with fixed execution period, then autonomy processes are fit into remaining slack time slots. We propose the use of quality-of-service (QoS) negotiation to explicitly trade off the performance of all processing tasks, including those related to spacecraft control. We characterize controller performance based on exhaustive search and a Lyapunov optimization technique and present results that analytically predict worst-case performance degradation characteristics. The results are illustrated by application to a second-order linear system with a linear state feedback control law.
Keywords
Lyapunov methods; aerospace control; linear systems; navigation; space vehicles; state feedback; Lyapunov optimization technique; QoS tradeoffs; complex dynamic events; control-related processes; fixed execution period; linear state feedback control law; mission goals; onboard autonomy; processing resources; second-order linear system; slack time slots; space missions; spacecraft control; worst-case performance degradation characteristics; Communication system control; Degradation; Linear systems; Navigation; Performance analysis; Process control; Processor scheduling; Quality of service; Space missions; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN
0-7803-7231-X
Type
conf
DOI
10.1109/AERO.2002.1035311
Filename
1035311
Link To Document