DocumentCode
2473237
Title
Correctness Analysis and Optimality Bounds of Multi-spacecraft Formation Initialization Algorithms
Author
Schuresko, Mike ; Cortés, Jorge
Author_Institution
Dept. of Appl. Math. & Stat., California Univ., Santa Cruz, CA
fYear
2006
fDate
13-15 Dec. 2006
Firstpage
5974
Lastpage
5979
Abstract
This paper considers formation initialization for a class of autonomous spacecraft operating in deep space with arbitrary initial positions and velocities. Formation initialization is the task of getting a group of autonomous agents to obtain the relative and/or global dynamic state information necessary to begin formation control. We associate a "worst-case total angle traversed" optimality notion with the execution of any formation initialization algorithm, and present performance bounds valid for any correct algorithm. We design the spatial spacecraft localization algorithm and the wait and check algorithm, analyze their correctness properties and characterize their performance in terms of worst-case optimality and execution time
Keywords
aerospace robotics; attitude control; mobile robots; multi-robot systems; position control; space vehicles; arbitrary initial position; autonomous spacecraft; correctness analysis; formation control; global dynamic state information; multispacecraft formation initialization algorithm; optimality bounds; relative dynamic state information; spatial spacecraft localization algorithm; wait and check algorithm; worst-case optimality; Algorithm design and analysis; Optimal control; Partitioning algorithms; Planets; Sensor phenomena and characterization; Space vehicles; Sun; USA Councils; Vehicle dynamics; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2006 45th IEEE Conference on
Conference_Location
San Diego, CA
Print_ISBN
1-4244-0171-2
Type
conf
DOI
10.1109/CDC.2006.377616
Filename
4177507
Link To Document