14 December 2016 Pointing system for the balloon-borne astronomical payloads
Kaipacheri Nirmal, Sreejith Aickara Gopinathan, Joice Mathew, Mayuresh Sarpotdar, Ambily Suresh, Ajin Prakash, Margarita Safonova, Jayant Murthy
Author Affiliations +
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.
Kaipacheri Nirmal, Sreejith Aickara Gopinathan, Joice Mathew, Mayuresh Sarpotdar, Ambily Suresh, Ajin Prakash, Margarita Safonova, and Jayant Murthy "Pointing system for the balloon-borne astronomical payloads," Journal of Astronomical Telescopes, Instruments, and Systems 2(4), 047001 (14 December 2016). https://doi.org/10.1117/1.JATIS.2.4.047001
Published: 14 December 2016
Lens.org Logo
CITATIONS
Cited by 7 scholarly publications.
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Sun

Astronomy

Sensors

Gyroscopes

Imaging systems

Control systems

Magnetometers

RELATED CONTENT

Attitude determination for balloon-borne experiments
Proceedings of SPIE (July 22 2014)
The feasibility of vision systems to form free space optical...
Proceedings of SPIE (September 25 2013)
Attitude control system evaluator for NASA sounding rockets
Proceedings of SPIE (November 02 1998)
F-SAT attitude stabilization system
Proceedings of SPIE (September 23 1993)
Mortar launched surveillance system
Proceedings of SPIE (February 21 2001)

Back to Top