TPF-I SWG Report - Exoplanet Exploration Program - NASA
TPF-I SWG Report - Exoplanet Exploration Program - NASA
TPF-I SWG Report - Exoplanet Exploration Program - NASA
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C HAPTER 6<br />
Figure 6-8: The Formation Control Testbed (FCT). Shown here are the two robots of the FCT, with<br />
Jason Keim. Each robot carries cannisters of compressed air that allow them to float off a polished metal<br />
floor. The floor is flat to within 2 one-thousandths of an inch (~50 μm) and spans a much larger area than<br />
shown here. The robots carry a platform (shown tilted for each robot) that is supported on a spherical ball<br />
bearing, also driven with compressed air so that the support of the platform is entirely frictionless. The<br />
robots serve as the hardware interface and testing ground for flight software developed for space<br />
applications in formation flying. The robots have completed their functional testing in cooperative mode<br />
and should achieve their major milestone of range and bearing control in mid 2007. The Principal<br />
Investigator of the Formation Control Testbed is Daniel Scharf.<br />
The robots are being tested within a celestarium that had been used previously to calibrate star trackers<br />
used by spacecraft. The spherical ceiling of the interior building has an array of artificial stars on it that<br />
the robot cameras can use to derive absolute position information down to the level necessary to reach the<br />
testbed's performance milestone.<br />
The FCT was planned as a ground-based laboratory consisting of three test robots in its fully deployed<br />
configuration. Much like in the distributed simulation under FAST, the FCT demonstrates formation<br />
acquisition, <strong>TPF</strong>-like formation maneuvering, and collision-free operations using the formation<br />
algorithms developed in the FAST. A high level of flight relevance was designed into the FCT avionics<br />
architecture, with on-board flight-like capabilities: (a) wireless communication emulating inter-spacecraft<br />
and spacecraft to ground communication; (b) on-board sensing and actuation using star tracker, gyros,<br />
thrusters, and reaction wheels for attitude and translation control; and (c) PowerPC flight control<br />
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