Three-axis control of tailless aircraft using fluidic actuators: MAGMA case study

Author:

Shearwood Thomas R.1,Nabawy Mostafa R.1,Crowther William J.1,Warsop Clyde2

Affiliation:

1. University of Manchester

2. BAE Systems

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Smith, D. R., and Warsop, C. "NATO AVT-239 Task Group: `Innovative Control Effectors for Manoeuvring of Air Vehicles' - Introduction and Overview," AIAA Scitech 2019 Forum, DOI: 10.2514/6.2019-0041.10.2514/6.2019-0041

2. Circulation control pneumatic aerodynamics: blown force and moment augmentation and modification - Past, present and future

3. Multi-effectors distribution of flying wing with stealthy optimization

4. Crowther, W., Lunnon, I., Shearwood, T., Llopis-pascual, A. Kabbabe, K., Altham, M., Forster, M., Knox, S., Harley, W., Bennetts, A., and Warsop, C. "Flight demonstration of fluidic controls on a tailless flight vehicle - an overview of the MAGMA programme Fluidic technologies," 2018, pp.24-26.

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