Structural load alleviation using distributed delay shaper: Application to flexible aircraft

Author:

Alam Mushfiqul,Hromcik Martin

Funder

Czech Technical University in Prague, Czechia

Czech Science Foundation (GACR), Czechia

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference39 articles.

1. Commissione europea : CORDIS : Progetti e risultati : Active Control for Flexible 2020 Aircraft;ACFA,2008

2. Alam, M. (2014). Combined feedforward/feedback gust load alleviation control for highly flexible aircraft. In Proceedings of 2014 PEGASUS-AIAA student conference. (pp. 1–12).

3. Active gust load alleviation system for flexible aircraft: Mixed feedforward/feedback approach;Alam;Aerospace Science and Technology,2015

4. Closed-form smoothers and shapers with distributed delay for damped oscillatory modes;Alikoç;IET Control Theory & Applications,2016

5. Unified aeroelastic and flight dynamic formulation via rational function approximations;Baldelli;Journal of Aircraft,2006

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