Skip to main content

HiDRON Measured Weather Conditions In The Stratosphere

By [email protected] - 6th February 2019 - 13:46

UAVOS Inc. and Stratodynamics Aviation Inc., have successfully completed the next stage of flights tests of the earth observation platform called the HiDRON to an altitude of 25 km (82,000 ft).

UAVOS Inc. and Stratodynamics Aviation Inc., have successfully completed the next stage of flights tests of the earth observation platform called the HiDRON to an altitude of 25 km (82,000 ft).

Aliaksei Stratsilatau, UAVOS Lead developer:
“We also undertook studies of the descending wind stream structure in the stratosphere to increase the duration of the HiDRON flight. In addition, our specialists developed a control and tracking system for an unmanned aircraft in real conditions within commercial air traffic space, which confirms the project’s readiness for commercial use.”

The high-altitude flight was conducted in collaboration with the regional Air Traffic Control Agency. The night-time flight was preferred to minimize impact on commercial air traffic. The HiDRON passed through commercial airspace twice, on the ascent and descent, and an adjustment to civilian aircraft routes was made during flight window. A backup UAVOS live-linked ground station and operator were stationed at the Air Traffic Control center, (multiple ground control stations can be synchronized from different locations). This enabled the mission team and air traffic control staff to track the aircraft’s position from the ground station and onboard transponder. Air traffic control staff indicated the transponder was sufficient for subsequent flights.

The HiDRON’s payload collected meteorological data and the atmospheric instruments were integrated with the autopilot telemetry and the sensors custom fitted to the aircraft. Data was collected at the ground station in real-time and compiled with the flight records. The instrument integration was also evaluated. While areas for further refinement were identified, the HiDRON and onboard measurement system performed well and demonstrated operability in high winds, cold temperatures, and low air density conditions. The obtained performance data will be used for the next stage of testing at an altitude of 30km (98,000 ft.).

Aliaksei Stratsilatau, UAVOS Lead developer:
“We also undertook studies of the descending wind stream structure in the stratosphere to increase the duration of the HiDRON flight. In addition, our specialists developed a control and tracking system for an unmanned aircraft in real conditions within commercial air traffic space, which confirms the project’s readiness for commercial use.”

The high-altitude flight was conducted in collaboration with the regional Air Traffic Control Agency. The night-time flight was preferred to minimize impact on commercial air traffic. The HiDRON passed through commercial airspace twice, on the ascent and descent, and an adjustment to civilian aircraft routes was made during flight window. A backup UAVOS live-linked ground station and operator were stationed at the Air Traffic Control center, (multiple ground control stations can be synchronized from different locations). This enabled the mission team and air traffic control staff to track the aircraft’s position from the ground station and onboard transponder. Air traffic control staff indicated the transponder was sufficient for subsequent flights.

Gary Pundsack, Stratodynamics Aviation Inc. Founder CEO:

“The HiDRON performed well in challenging winter winds and night conditions. At the 25km launch altitude, the HiDRON travelled 36 km from home. The return glide was controlled and, at an altitude of 18 km, the HIDRON was above the home position where it loitered in a slow descent down. Even with a build-up of ice on the wings, from passing through low-level clouds, the HiDRON landed autonomously. The test demonstrated the HiDRON’s aerodynamic capabilities and avionic system reliability.”

How it works?
The HiDRON, a joint project of UAVOS Inc. and Stratodynamics Aviation Inc., is a fixed wing glider integrated with meteorological equipment and launched by a stratospheric helium-filled weather balloon. With 3.4 m wingspan, the HiDRON weighs under 5 kg and is capable of carrying an in-situ measurement instrument weighing up to 1 kg. Data from the integrated instrument is transmitted via telemetry immediately and during the ascent into the stratosphere to a ground station, (much like a typical weather radiosonde). After reaching an altitude of 25 km, set by the ground station operator, the HiDRON disconnects from the balloon and glides back to the specified landing site. Changes to the flight plan can be made by the operator in real-time. To increase the flight duration, algorithms automatically process efficient flight controls to maintain optimal energy. Aircraft landing is fully automatic.

All operational parameters are transmitted via radio telemetry with a range of 100 km (66 mi.). An iridium satellite link provides a back-up communication system. Other safety features include a deployable parachute and a dual redundant balloon release system.

Marcelo Guzman and Travis Schuyler, University of Kentucky, Researchers

“A project goal is to better understand meteorological and weather forecasting models by measuring atmospheric conditions during high-altitude aerial vehicle flights, and we are very excited to share the data collected using the HiDRON with the Scientific community,” commented Marcelo Guzman. Travis Schuyler added, “This is the first time that this kind of atmospheric-sensing equipment has been integrated into a balloon-launched, unmanned glider and the results will enable the evolution of new UAV technology and in-situ observation methodologies.”

Read More: Climate Change Data Capture Satellite Positioning, Navigation & Timing (PNT) Cartography Autonomous Underwater Vehicles Unmanned Aerial Vehicles Education & Research Environmental

Subscribe to our newsletter

Stay updated on the latest technology, innovation product arrivals and exciting offers to your inbox.

Newsletter