Grant: Alliance Grants
University of Waterloo
$94,666.00
Research and development of key aerodynamics and communication components for a new unmanned stratospheric glider
EF 2021-22
Résumé
The main goal of this project is to enable the design and deployment of a novel unmanned glider platform for stratospheric flight. The glider will be launched via a lighter-than-air balloon to deliver up to 5 kg of payload to an altitude of approximately 35 km, where it will be released for the desired data collection during an autonomously controlled descent to a set location. The project is performed in collaboration with Statodynamics Aviation Inc., who provides unique high-altitude flight services for a wide arrange of earth observation, testing, and monitoring missions using autonomous aerial vehicles. The new glider platform is aimed to address the rapidly growing demand for cost-effective, high-altitude measurements required for a variety of earth observation missions, including atmosphere sampling, meteorological measurements, and monitoring of local environmental pollution, as well as calibration of surface- and space-based communication equipment and technology development prior to space deployment. It offers significant advantages over the currently used free-drift probes by providing controlled tests capabilities, ensuring payload retrieval, and significantly reducing the environmental footprint. However, the design of such a glider is associated with unique, multidisciplinary research challenges in the areas of aerodynamics and communications, which are addressed in the present proposal. The results will enable controlled glider operation over an unprecedently wide range of operating conditions, provide reliable positioning and control, and ensure robust communication and data transfer.
Programme
Alliance Grants
Bénéficiaire
Emplacement
Ontario, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
562020-2021
Name nom
Yarusevych, Serhiy
Department département
Mechanical Engineering and Mechatronics
Organization id
33
Institution établissement
University of Waterloo
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2021
Competition year année de concours
2021
Award amount
94666
Program id
ALLRP
Program name en
Alliance Grants
Program name fr
Subventions Alliance
Group en
Research partnerships programs
Group fr
Programmes de partenariat
Committee code
96
Committee name en
RPP Internal Decision Cttee
Committee name fr
Cté de décision interne - PPR
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2200
Research subject group en
Fluid mechanics
Research subject group fr
Mécanique des fluides
Research subject en
Fluid mechanics
Research subject fr
Mécanique des fluides
Installment
inst:1
Partie
1
Nb partie
3
Application title
Research and development of key aerodynamics and communication components for a new unmanned stratospheric glider
Keyword
NSERC
Application summary
The main goal of this project is to enable the design and deployment of a novel unmanned glider platform for stratospheric flight. The glider will be launched via a lighter-than-air balloon to deliver up to 5 kg of payload to an altitude of approximately 35 km, where it will be released for the desired data collection during an autonomously controlled descent to a set location. The project is performed in collaboration with Statodynamics Aviation Inc., who provides unique high-altitude flight services for a wide arrange of earth observation, testing, and monitoring missions using autonomous aerial vehicles. The new glider platform is aimed to address the rapidly growing demand for cost-effective, high-altitude measurements required for a variety of earth observation missions, including atmosphere sampling, meteorological measurements, and monitoring of local environmental pollution, as well as calibration of surface- and space-based communication equipment and technology development prior to space deployment. It offers significant advantages over the currently used free-drift probes by providing controlled tests capabilities, ensuring payload retrieval, and significantly reducing the environmental footprint. However, the design of such a glider is associated with unique, multidisciplinary research challenges in the areas of aerodynamics and communications, which are addressed in the present proposal. The results will enable controlled glider operation over an unprecedently wide range of operating conditions, provide reliable positioning and control, and ensure robust communication and data transfer.