Time-Domain System Identification of Helicopters Using Nonlinear Acceleration and Jerk Prediction Model-Reference-Cited by-同舟云学术

Time-Domain System Identification of Helicopters Using Nonlinear Acceleration and Jerk Prediction Model

Published:2019-05 Issue:3 Volume:56 Page:1272-1280
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Setu Sagar¹,Abhishek Abhishek¹,Venkatesan C.¹

Affiliation:

1. Indian Institute of Technology Kanpur, Kanpur 208 016, India

Funder

Department of Science and Technology, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035273

Reference28 articles.

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3. Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage Dynamics

4. TischlerM. B.RempleR. K. “Aircraft and Rotorcraft System Identification,” AIAA, Reston, VA, 2006, pp. 83–450. doi:10.2514/4.868207

5. Development of a Full Flight Envelope Helicopter Simulation Using System Identification

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