Laser and vision-based measurements of helicopter blade angles

Author:

Zappa EmanueleORCID,Liu Rui,Trainelli Lorenzo,Ferrario Andrea,Cordisco Potito,Terraneo Mauro,Grassetti Riccardo,Redaelli Matteo

Funder

MANOEUVRES

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Reference43 articles.

1. Rotor-state feedback in the design of flight control laws for a hovering helicopter;Takahashi;J. Am. Helicopter Soc.,1994

2. C.M. Ivler, Development and comparison of explicit and implicit rotor-state feedback control systems for a Fly-by-Wire UH-60, AHS Rotorcraft Handling Qualities Specialists’ Meeting, Huntsville, U.S.A., February, 2014.

3. P. Cordisco, R. Liu, M. Redaelli, et al., Developing a novel contactless sensor for helicopter rotor state measurements, in: 36th European Telemetry and Test Conference ETC2016 – 3rd Symposium on Advanced In-flight Measurement Techniques AIM2016, Nuremberg, Germany, May, 2016.

4. Innovative helicopter in-flight noise monitoring enabled by rotor state measurements;Trainelli;Noise Mapping,2016

5. D.A. Barrows, A.W. Burner, A.I. Abrego, et al., Blade displacement measurements of the full-scale UH-60A airloads rotor, in: 29th AIAA Applied Aerodynamics Conference, Hawaii, U.S.A., June, 2011.

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