Aeroservoelastic modelling and control of a slender anti-air missile for active damping of longitudinal bending vibrations-Reference-Cited by-同舟云学术

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Aeroservoelastic modelling and control of a slender anti-air missile for active damping of longitudinal bending vibrations

Published:2017-07 Issue: Volume:66 Page:20-27
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Verhaegen Anatole,Żbikowski Rafał

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. Phase vs. gain stabilization of structural feedback oscillations in homing missile autopilots;Nesline,1985

2. Aeroelastic stability of slender, spinning missiles;Platus;J. Guid. Control Dyn.,1992

3. Flight mechanics of an elastic symmetric missile;Murphy;J. Guid. Control Dyn.,2001

4. Aeroservoelastic stability of supersonic slender-body flight vehicles;Haddadpour;J. Guid. Control Dyn.,2006

5. Aeroelastic behavior of a slender body considering free fittings;Ehramianpour;J. Mech. Sci. Technol.,2010

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2. Aeroelastic Response of Spinning Projectiles with Large Slenderness Ratio at Supersonic Speed;Aerospace;2023-07-18

3. Aeroservoelastic Stability Evaluation for Slender Vehicles Based on the Ground Frequency Response Test;Aerospace;2022-12-19

4. A fast and accurate transfer alignment method without relying on the empirical model of angular deformation;Journal of Navigation;2022-06-01

5. Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-12-17

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