The TARDIS experiment: An innovative VOR-based system for HAPS backup positioning and attitude determination

TARDIS (Tracking and Attitude Radio-based Determination In Stratosphere) is a stratospheric experiment that exploits the VHF Omnidirectional Range (VOR) signal to perform an in-flight attitude and position determination. This project has been conceived by a group of students of Aerospace Engineering...

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Bibliographic Details
Main Authors: Bandini V., di Palo L., Bedetti E., Broggi G., Celesti P., Collettini L., di Ienno D., Garofalo R., Iovanna F., Mattei G., Vestito E., Gianfermo A., Marzioli P.
Other Authors: Bandini, V., di Palo, L., Bedetti, E., Broggi, G., Celesti, P., Collettini, L., di Ienno, D., Garofalo, R., Iovanna, F., Mattei, G., Vestito, E., Gianfermo, A., Marzioli, P.
Format: Conference Object
Language:English
Published: International Astronautical Federation, IAF 2019
Subjects:
VOR
Online Access:http://hdl.handle.net/11573/1493891
Description
Summary:TARDIS (Tracking and Attitude Radio-based Determination In Stratosphere) is a stratospheric experiment that exploits the VHF Omnidirectional Range (VOR) signal to perform an in-flight attitude and position determination. This project has been conceived by a group of students of Aerospace Engineering from Sapienza University of Rome and selected for the Rocket and Balloon Experiments for University Students (REXUS/BEXUS) Programme cycle 12. The programme is managed by the Swedish Space Agency (SNSA) and the German Space Agency (DLR) in collaboration with the European Space Agency (ESA). The experiment will be launched from Esrange Space Centre in Kiruna (Sweden) in October 2019. VOR is a radio-navigation systems based on high power transmitting stations at ground and on passive airborne receivers. The navigational information decoded by the receivers is defined as “radial” and it represents the bearing angle of the receiver with respect to the ground station position. The balloon position is obtained by the integration of two radials. An attitude estimation can be done through the pseudo-doppler radio direction finding method with four different antennas electrically switched by a RF PCB. This process will give the signal source direction and integrated with the balloon position, it will determine the attitude. The investigation could demonstrate the applicability of a passive system, based on a mature ground-based radio-frequency infrastructure, for the implementation as back-up position and attitude determination for the future stratospheric vehicles. High Altitude Platform Stations (HAPS), planned to autonomously operate for months, could implement such a system for improving the reliability of their navigation systems.