Co-design of aircraft vertical tail and control laws with distributed electric propulsion and flight envelop constraints

Author:

Nguyen Van EricORCID,Alazard Daniel,Döll Carsten,Pastor Philippe

Funder

Airbus

ONERA

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference27 articles.

1. Nguyen-Van, E., Alazard, D., Döll, C.: Co-design of aircraft vertical tail and control laws using distributed electric propulsion. IFAC-PapersOnLine 52(12), 514–519 (2019). https://doi.org/10.1016/j.ifacol.2019.11.295 (21st IFAC Symposium on Automatic Control in Aerospace ACA 2019)

2. Hermetz, J., Ridel, M., Döll, C.: Distributed Electric Propulsion for small business aircraft—a concept-plane for key-technologies investigations. In: Proc. 30th ICAS Congress. Daejeon (2016)

3. Bushnell, D.M.: Aircraft drag reduction—a review. J. Aerosp. Eng. 217(1) (2003)

4. Ko, A., Schetz, J.A., Mason, W.H.: Assessment of the potential advantages of distributed propulsion for aircraft. ISABE-2003-1094 (2003)

5. Ameyugo, G., Taylor, M., Singh, R.: Distributed propulsion feasibility studies. ICAS06 (2006)

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