TY - GEN
T1 - Modified equations of motion around circular trajectory and its application to formation flying control
AU - Kawaguchi, Jun'ichiro
PY - 2007
Y1 - 2007
N2 - Usually, the formation flying associated with a circular orbit is discussed through the well-known Hill's equations of motion. This paper presents and discusses the formation-fixed coordinate to discuss about the formation behavior. The resulted equations take the non-autonomous form and will depict some interesting characteristics. The paper will also present the application of decentralized formation control strategy that stabilizes and enables a quick reaction to the command.
AB - Usually, the formation flying associated with a circular orbit is discussed through the well-known Hill's equations of motion. This paper presents and discusses the formation-fixed coordinate to discuss about the formation behavior. The resulted equations take the non-autonomous form and will depict some interesting characteristics. The paper will also present the application of decentralized formation control strategy that stabilizes and enables a quick reaction to the command.
UR - http://www.scopus.com/inward/record.url?scp=55849083969&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=55849083969&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:55849083969
SN - 9780877035411
T3 - Advances in the Astronautical Sciences
SP - 1429
EP - 1434
BT - American Astronautical Society - Space Flight Mechanics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Space Flight Mechanics Meeting
T2 - 17th Annual Space Flight Mechanics Meeting
Y2 - 28 January 2007 through 1 February 2007
ER -