Propulsion control design for a STOVL Integrated Flight/Propulsion Control system

Watts, Stephen R.; Larkin, Louis J.; Hill, Brian; Wood, Charles Cresson

doi:10.2514/6.1993-4868

International Powered Lift Conference 1993

DOI: 10.2514/6.1993-4868

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Propulsion control design for a STOVL Integrated Flight/Propulsion Control system

Stephen R. Watts

Louis J. Larkin

Brian Hill

et al.

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2024

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Multi-nozzle thrust matching control of STOVL engine

Pang,

Fu,

et al. 2024

International Journal of Turbo &Amp; Jet-Engines

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A multi-nozzle thrust matching control method is proposed in this paper to provide the thrust vector required of lift-fan type short takeoff and vertical landing (STOVL) aircrafts during hover. Attitude-matched thrust commands for each nozzle of STOVL engine are generated based on a six-degree-of-freedom aircraft model. The thrust controller is divided into two blocks according to the coupling analysis. Based on the combination of linear matrix inequality and differential evolution algorithm, a multi-target controller parameters optimization method is proposed to achieve stable disturbance suppression and fast command tracking. Simulations results show that the proposed command generated model is effective and the decoupling control method can effectively suppress the coupling between the loops and realize the matching control of thrust.

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Multi-nozzle thrust matching control of STOVL engine

Pang,

Fu,

et al. 2024

International Journal of Turbo &Amp; Jet-Engines

View full text Add to dashboard Cite

show abstract

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Propulsion control design for a STOVL Integrated Flight/Propulsion Control system

Cited by 1 publication

References 1 publication

Multi-nozzle thrust matching control of STOVL engine

Multi-nozzle thrust matching control of STOVL engine

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