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Field of Research : Aircraft performance and flight control systems
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Aircraft performance and flight control systems (3)
Aerospace engineering (2)
Electrochemical energy storage and conversion (2)
Flight dynamics (2)
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Control engineering mechatronics and robotics (1)
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  • Active Funded Activity

    Discovery Projects - Grant ID: DP240101140

    Funder
    Australian Research Council
    Funding Amount
    $518,252.00
    Summary
    Insect-inspired flapping wing robots: autonomous flight control systems. This project aims to design a novel control scheme for insect-inspired, flapping-wing, micro aerial vehicles. This type of micro aerial vehicle has complex, periodic, time-varying and inherently unstable dynamics, which are practically challenging to model and implement in hardware. This project will design energy-based automatic stabilization and task-dependent control, and develop the insect-inspired platform for testing .... Insect-inspired flapping wing robots: autonomous flight control systems. This project aims to design a novel control scheme for insect-inspired, flapping-wing, micro aerial vehicles. This type of micro aerial vehicle has complex, periodic, time-varying and inherently unstable dynamics, which are practically challenging to model and implement in hardware. This project will design energy-based automatic stabilization and task-dependent control, and develop the insect-inspired platform for testing nonlinear control strategies. The expected outcomes will include new system and control theories, concepts, principles and technologies in controller design that can provide reliable flight control for bio-inspired, flapping-wing systems.
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    Active Funded Activity

    Mid-Career Industry Fellowships - Grant ID: IM230100644

    Funder
    Australian Research Council
    Funding Amount
    $889,472.00
    Summary
    Triple hybrid fuel-cell-based propulsion for long-range eVTOL operations. AMSL Aero's Vertiia is an Australian-developed electric Vertical Take Off and Landing (eVTOL) aircraft that will provide rapid response air ambulance and low-cost passenger transport for rural Australia. This project will optimise a fuel cell/battery/ultracapacitor triple hybrid system for Vertiia by combining dynamic energy source models, hardware-in-the-loop simulations, aero-propulsive flight mechanics models, and accel .... Triple hybrid fuel-cell-based propulsion for long-range eVTOL operations. AMSL Aero's Vertiia is an Australian-developed electric Vertical Take Off and Landing (eVTOL) aircraft that will provide rapid response air ambulance and low-cost passenger transport for rural Australia. This project will optimise a fuel cell/battery/ultracapacitor triple hybrid system for Vertiia by combining dynamic energy source models, hardware-in-the-loop simulations, aero-propulsive flight mechanics models, and accelerated degradation testing. The triple hybrid will extend the life of both batteries and fuel cells for eVTOL aircraft. It will allow AMSL to fast-track the improved durability needed for cost-competitive long-range eVTOL operations, giving them an up-front and industry-leading experience on hybrid systems for eVTOLs.
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    Active Funded Activity

    ARC Future Fellowships - Grant ID: FT230100519

    Funder
    Australian Research Council
    Funding Amount
    $1,118,292.00
    Summary
    Energy Source Durability for Electric Vertical TakeOff and Landing Aircraft. This project aims to address energy source durability for electric Vertical Take Off and Landing (eVTOL) aircraft by optimising a fuel cell/battery/ultracapacitor triple hybrid energy system. The project expects to generate new knowledge in the area of energy source durability using interdisciplinary approaches that combine energy source degradation models, hardware-in-the-loop simulations, aero-propulsive flight mechan .... Energy Source Durability for Electric Vertical TakeOff and Landing Aircraft. This project aims to address energy source durability for electric Vertical Take Off and Landing (eVTOL) aircraft by optimising a fuel cell/battery/ultracapacitor triple hybrid energy system. The project expects to generate new knowledge in the area of energy source durability using interdisciplinary approaches that combine energy source degradation models, hardware-in-the-loop simulations, aero-propulsive flight mechanics models, and accelerated degradation testing. This should provide significant benefits, allowing to fast-track the improved longevity needed for cost-competitive long-range rapid response air ambulance eVTOL operations.
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    Showing 1-3 of 3 Funded Activites

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