Precise Pointing and Stabilization Performance for the Balloon-borne Imaging Testbed (BIT): 2015 Test Flight
L. J. Romualdez, P. Clark, C. J. Damaren, M. N. Galloway, J. W., Hartley, L. Li, R. J. Massey, C. B. Netterfield

TL;DR
This paper reports on the design, implementation, and successful testing of the attitude control system for the Balloon-borne Imaging Testbed, achieving high-precision pointing and stabilization during a 2015 test flight, with plans for further improvements.
Contribution
It presents a detailed analysis of the ADCS performance for the BIT, demonstrating sub-arcsecond stabilization in a balloon-borne astronomy platform and outlining enhancements for future flights.
Findings
Pointing stability of 0.68 arcseconds (rms) achieved during flight.
Coarse pointing accuracy within 0.1 degrees.
System modifications planned for improved future performance.
Abstract
Balloon-borne astronomy offers an attractive option for experiments that require precise pointing and attitude stabilization, due to a large reduction in the atmospheric interference observed by ground-based systems as well as the low-cost and short development time-scale compared to space-borne systems. The Balloon-borne Imaging Testbed (BIT) is an instrument designed to meet the technological requirements of high precision astronomical missions and is a precursor to the development of a facility class instrument with capabilities similar to the Hubble Space Telescope. The attitude determination and control systems (ADCS) for BIT, the design, implementation, and analysis of which are the focus of this paper, compensate for compound pendulation effects and other sub-orbital disturbances in the stratosphere to within 1-2 (rms), while back-end optics provide further image…
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Taxonomy
TopicsInertial Sensor and Navigation · Infrared Target Detection Methodologies · Adaptive optics and wavefront sensing
