Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model Export

@article{citeulike:1277548, abstract = {This article deals with design and realisation of a canard foreplane control system for an aeroelastic demonstrator, suitable for wind tunnel testing. Hardware and software will be described as the methodology adopted to design, implement and realise the software. Specific attention is devoted to PID application, tuning and fuselage vibration control implementation. Results of preliminary test and simulations are presented and show realistic system effectiveness in damping fuselage bending and torsion. This work describes all the activity performed at Politecnico di Milano before wind tunnel testing at VZLU, Prague, as part of Active Aeroelastic Aircraft Structures (3AS) EU project.}, author = {Ricci, S. and Scotti, A. and Zanotti, D.}, citeulike-article-id = {1277548}, citeulike-linkout-0 = {http://www.sciencedirect.com/science/article/B6WN1-4H98T24-1/2/efd7c06438f0ff4324de07d602688082}, journal = {Mechanical Systems and Signal Processing}, keywords = {40051041, aeroelastic, bending, foreplane, fuselage, system, torsion, tunnel, vibration}, month = {July}, number = {5}, pages = {1044--1066}, posted-at = {2007-05-09 22:02:57}, priority = {4}, title = {Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model}, url = {http://www.sciencedirect.com/science/article/B6WN1-4H98T24-1/2/efd7c06438f0ff4324de07d602688082}, volume = {20}, year = {2006} }

TY - JOUR ID - citeulike:1277548 L3 - citeulike-article-id:1277548 N2 - This article deals with design and realisation of a canard foreplane control system for an aeroelastic demonstrator, suitable for wind tunnel testing. Hardware and software will be described as the methodology adopted to design, implement and realise the software. Specific attention is devoted to PID application, tuning and fuselage vibration control implementation. Results of preliminary test and simulations are presented and show realistic system effectiveness in damping fuselage bending and torsion. This work describes all the activity performed at Politecnico di Milano before wind tunnel testing at VZLU, Prague, as part of Active Aeroelastic Aircraft Structures (3AS) EU project. IS - 5 JF - Mechanical Systems and Signal Processing EP - 1066 TI - Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model VL - 20 SP - 1044 KW - 40051041 KW - aeroelastic KW - bending KW - foreplane KW - fuselage KW - system KW - torsion KW - tunnel KW - vibration AU - Ricci, S AU - Scotti, A AU - Zanotti, D PY - 2006/07// UR - http://www.sciencedirect.com/science/article/B6WN1-4H98T24-1/2/efd7c06438f0ff4324de07d602688082 ER -