# The EBEX Balloon-Borne Experiment - Gondola, Attitude Control, and   Control Software

**Authors:** The EBEX Collaboration: Asad Aboobaker, Peter Ade, Derek Araujo,, Fran\c{c}ois Aubin, Carlo Baccigalupi, Chaoyun Bao, Daniel Chapman, Joy, Didier, Matt Dobbs, Will Grainger, Shaul Hanany, Kyle Helson, Seth Hillbrand,, Johannes Hubmayr, Andrew Jaffe, Bradley Johnson, Terry Jones, Jeff Klein,, Andrei Korotkov, Adrian Lee, Lorne Levinson, Michele Limon, Kevin MacDermid,, Amber D. Miller, Michael Milligan, Lorenzo Moncelsi, Enzo Pascale, Kate, Raach, Britt Reichborn-Kjennerud, Ilan Sagiv, Carole Tucker, Gregory S., Tucker, Benjamin Westbrook, Karl Young, Kyle Zilic

arXiv: 1702.07020 · 2018-11-14

## TL;DR

The EBEX balloon experiment successfully integrated advanced detector technology and innovative control software to measure CMB polarization, demonstrating reliable operation and precise attitude control during its long-duration flight.

## Contribution

First balloon-borne CMB experiment to implement a kilo-pixel TES array with digital frequency domain multiplexing and specialized attitude software.

## Key findings

- Faultless TES array management during flight
- Effective power and cooling systems for detectors
- Attitude reconstruction errors below 10% of B-mode signal

## Abstract

The E and B Experiment (EBEX) was a long-duration balloon-borne instrument designed to measure the polarization of the cosmic microwave background (CMB) radiation. EBEX was the first balloon-borne instrument to implement a kilo-pixel array of transition edge sensor (TES) bolometric detectors and the first CMB experiment to use the digital version of the frequency domain multiplexing system for readout of the TES array. The scan strategy relied on 40 s peak-to-peak constant velocity azimuthal scans. We discuss the unique demands on the design and operation of the payload that resulted from these new technologies and the scan strategy. We describe the solutions implemented including the development of a power system designed to provide a total of at least 2.3 kW, a cooling system to dissipate 590 W consumed by the detectors' readout system, software to manage and handle the data of the kilo-pixel array, and specialized attitude reconstruction software. We present flight performance data showing faultless management of the TES array, adequate powering and cooling of the readout electronics, and constraint of attitude reconstruction errors such that the spurious B-modes they induced were less than 10% of CMB B-mode power spectrum with $r=0.05$.

## Full text

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## Figures

7 figures with captions in the complete paper: https://tomesphere.com/paper/1702.07020/full.md

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Source: https://tomesphere.com/paper/1702.07020