Search Results - Zaludin, Zairil

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  1. 1
    Integration of Luenberger estimator with control reconfiguration system for hypersonic aircraft

    Integration of Luenberger estimator with control reconfiguration system for hypersonic aircraft by Zaludin, Zairil

    Published 2023
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  2. 2
    Drone fault tolerance strategy by allowing remaining rotor to pan and tilt

    Drone fault tolerance strategy by allowing remaining rotor to pan and tilt by Zaludin, Zairil

    Published 2024
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  3. 3
    Control revert system.

    Control revert system. by Zaludin, Zairil Azhar

    Published 2007
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  4. 4
    Concept paper: why managing universities like entrepreneurs will solve financial problems in institutions of higher learning

    Concept paper: why managing universities like entrepreneurs will solve financial problems in institutions of higher learning by Zaludin, Zairil Azhar

    Published 2019
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  5. 5
    Fault tolerance conceptual strategy for a quadcopter drone with rotor failure

    Fault tolerance conceptual strategy for a quadcopter drone with rotor failure by Zaludin, Zairil A.

    Published 2023
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  6. 6
    Sensor and process noises reduction using a Luenberger state estimator with a stability augmentation system for a Hypersonic Transport Aircraft

    Sensor and process noises reduction using a Luenberger state estimator with a stability augmentation system for a Hypersonic Transport Aircraft by Zaludin, Zairil A.

    Published 2022
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  7. 7
    Concept paper: kaizen principles in aerospace education

    Concept paper: kaizen principles in aerospace education by Zaludin, Zairil Azhar, Derasol, Kamariah

    Published 2019
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  8. 8
    Automatic flight control requirements for transition flight phases when converting long endurance fixed wing UAV to VTOL aircraft

    Automatic flight control requirements for transition flight phases when converting long endurance fixed wing UAV to VTOL aircraft by Zaludin, Zairil Azhar, Gires, Ezanee

    Published 2019
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  9. 9
    The use of a negative definite state-weighting matrix in linear optimal aircraft stability augmentation system problems

    The use of a negative definite state-weighting matrix in linear optimal aircraft stability augmentation system problems by Zaludin, Zairil Azhar, McLean, Donald

    Published 2001
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  10. 10
    Challenges and trends of changing from hover to forward flight for a converted hybrid fixed wing VTOL UAS from automatic flight control system perspective

    Challenges and trends of changing from hover to forward flight for a converted hybrid fixed wing VTOL UAS from automatic flight control system perspective by Zaludin, Zairil Azhar, Mohd Harithuddin, Ahmad Salahuddin

    Published 2019
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