Pointing system for the balloon-borne astronomical payloads

Kaipacheri Nirmal; Aickara Gopinathan Sreejith; Joice Mathew; Mayuresh Sarpotdar; Suresh Ambily; Ajin Prakash; Margarita Safonova; Jayant Murthy

doi:10.1117/1.JATIS.2.4.047001

Pointing system for the balloon-borne astronomical payloads

Kaipacheri Nirmal^*, Aickara Gopinathan Sreejith, Joice Mathew, Mayuresh Sarpotdar, Suresh Ambily, Ajin Prakash, Margarita Safonova, Jayant Murthy

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

9 Citations (Scopus)

Abstract

We describe the development and implementation of a light-weight, fully autonomous 2-axis pointing and stabilization system designed for balloon-borne astronomical payloads. The system is developed using off-the-shelf components such as Arduino Uno controller, HMC 5883L magnetometer, MPU-9150 inertial measurement unit, and iWave GPS receiver unit. It is a compact and rugged system which can also be used to take images/video in a moving vehicle or in real photography. The system performance is evaluated from the ground, as well as in conditions simulated to imitate the actual flight by using a tethered launch.

Original language	English
Article number	047001
Journal	Journal of Astronomical Telescopes, Instruments, and Systems
Volume	2
Issue number	4
DOIs	https://doi.org/10.1117/1.JATIS.2.4.047001
Publication status	Published - 1 Oct 2016
Externally published	Yes

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title = "Pointing system for the balloon-borne astronomical payloads",

abstract = "We describe the development and implementation of a light-weight, fully autonomous 2-axis pointing and stabilization system designed for balloon-borne astronomical payloads. The system is developed using off-the-shelf components such as Arduino Uno controller, HMC 5883L magnetometer, MPU-9150 inertial measurement unit, and iWave GPS receiver unit. It is a compact and rugged system which can also be used to take images/video in a moving vehicle or in real photography. The system performance is evaluated from the ground, as well as in conditions simulated to imitate the actual flight by using a tethered launch.",

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AU - Nirmal, Kaipacheri

AU - Sreejith, Aickara Gopinathan

AU - Mathew, Joice

AU - Sarpotdar, Mayuresh

AU - Ambily, Suresh

AU - Prakash, Ajin

AU - Safonova, Margarita

AU - Murthy, Jayant

PY - 2016/10/1

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N2 - We describe the development and implementation of a light-weight, fully autonomous 2-axis pointing and stabilization system designed for balloon-borne astronomical payloads. The system is developed using off-the-shelf components such as Arduino Uno controller, HMC 5883L magnetometer, MPU-9150 inertial measurement unit, and iWave GPS receiver unit. It is a compact and rugged system which can also be used to take images/video in a moving vehicle or in real photography. The system performance is evaluated from the ground, as well as in conditions simulated to imitate the actual flight by using a tethered launch.

AB - We describe the development and implementation of a light-weight, fully autonomous 2-axis pointing and stabilization system designed for balloon-borne astronomical payloads. The system is developed using off-the-shelf components such as Arduino Uno controller, HMC 5883L magnetometer, MPU-9150 inertial measurement unit, and iWave GPS receiver unit. It is a compact and rugged system which can also be used to take images/video in a moving vehicle or in real photography. The system performance is evaluated from the ground, as well as in conditions simulated to imitate the actual flight by using a tethered launch.

KW - attitude sensor

KW - balloon experiment

KW - microelectromechanical system sensors

KW - pointing system

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M3 - Article

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JO - Journal of Astronomical Telescopes, Instruments, and Systems

JF - Journal of Astronomical Telescopes, Instruments, and Systems

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Pointing system for the balloon-borne astronomical payloads

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