https://murray.cds.caltech.edu/index.php?action=history&feed=atom&title=Constrained_Trajectory_Generation_for_Microsatellite_Formation_FlyingConstrained Trajectory Generation for Microsatellite Formation Flying - Revision history2026-09-10T03:14:41ZRevision history for this page on the wikiMediaWiki 1.44.2https://murray.cds.caltech.edu/index.php?title=Constrained_Trajectory_Generation_for_Microsatellite_Formation_Flying&diff=19965&oldid=prevMurray: htdb2wiki: creating page for 2001b_mpm01-gnc.html2016-05-15T06:19:19Z<p>htdb2wiki: creating page for 2001b_mpm01-gnc.html</p>
<p><b>New page</b></p><div>{{HTDB paper<br />
| authors = Mark B. Milam, Nicolas Petit and Richard M. Murray<br />
| title = Constrained Trajectory Generation for Microsatellite Formation Flying<br />
| source = Submitted, 2001 AIAA Guidance, Navigation and Control Conference<br />
| year = 2001<br />
| type = Conference <br />
Paper<br />
| funding = AFOSR<br />
| url = http://www.cds.caltech.edu/~murray/preprints/mpm01-gnc.pdf<br />
| abstract = Station keeping and reorientation control of a cluster of fully-actuated <br />
low-thrust micro-satellites is considered in this paper. We address the control <br />
problem by taking advantage of the fully-actuated structure of the micro-satellite. <br />
We propose a very general open-loop solution by solving in real-time constrained <br />
trajectory generation problems for stationkeeping and reorientation. Performance <br />
of this methodology is reported for a typical micro-satellite format ion flying <br />
space mission using the Nonlinear Trajectory Generation software package. <br />
| flags = <br />
| tag = mpm01-gnc<br />
| id = 2001b<br />
}}</div>Murray