A Control Allocation approach to induce the center of pressure position and shape the aircraft transient response-Reference-Cited by-同舟云学术

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A Control Allocation approach to induce the center of pressure position and shape the aircraft transient response

Published:2021-12 Issue: Volume:119 Page:107092
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Varriale Carmine^ORCID,Voskuijl Mark

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Design of the blended wing body subsonic transport;Liebeck;J. Aircr.,2004

2. The effect of engine location on the aerodynamic efficiency of a flying-v aircraft;Pascual,2020

3. Induced Drag of Multiplanes;Prandtl,1924

4. Minimum induced drag theorems for multi-wing systems;Demasi,2016

5. The PrandtlPlane configuration: overview on possible applications to civil aviation;Frediani,2012

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1. A CFD-Based Collaborative Approach for Box-Wing Aircraft Aerodynamic Assessment: The PARSIFAL Study Case;Aerotecnica Missili & Spazio;2023-09-17

2. Test mass 6-DOF control allocation based on the null space for space gravitational wave mission;Aerospace Science and Technology;2023-09

3. Flight Performance Evaluation of the Flying-V;AIAA AVIATION 2023 Forum;2023-06-08

4. Impact of Control Allocation Methods on the Design of Control Surface Layouts for Box-Wing Aircraft under Flying Qualities Constraints;AIAA AVIATION 2023 Forum;2023-06-08

5. Linear quadratic regulator based on extended state observer–based active disturbance rejection control of autonomous vehicle path following control;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2022-09-07

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