Control of Unsteady Aeroelastic System via State-Dependent Riccati Equation Method

By Nilesh Bhoir, Sahjendra N. Singh. 2005

58 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/68d017d8acebd480feb80c7e4861a5701a38e971

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Tayfun Çimen

In Computational Mechanics

1. Tayfun Çimen

In Control and Systems Engineering

1. Tayfun Çimen
2. Rajarshi Bardhan
3. Debasish Ghose

Citations in the corpus

• Survey of State-Dependent Riccati Equation in Nonlinear Optimal Feedback Control Synthesis (2012, background): “b) The second contribution is flutter suppression of aeroelastic wing sections using full-state and/or partial-state feedback [49–51].”