Experimental Investigation of Real-Time Helicopter Weight Estimation-Reference-Cited by-同舟云学术

Experimental Investigation of Real-Time Helicopter Weight Estimation

Published:2014-05 Issue:3 Volume:51 Page:1047-1051
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Taylor Bradley¹,Rogers Jonathan²

Affiliation:

1. Department of Aerospace Engineering, Texas A&M University, College Station, Texas 77843

2. Woodruff School of Mechanical Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032449

Reference13 articles.

1. MoffattJ. G. “Helicopter Gross Weight Determination from Monitored Parameters,” U.S. Army Aviation and Troop Command TR-96-D-5, Fort Eustis, VA, May 1996.

2. Numerical Study on the Robustness of a Neural Network Model for Gross Weight Estimation of Tiltrotor Aircraft

3. In-Flight Weight and Balance Identification Using Neural Networks

4. In-Flight Estimation of Helicopter Gross Weight and Mass Center Location

5. TalbotP. D.TinlingB. E.DeckerW. A.ChenR. T. N. “A Mathematical Model of a Single Main Rotor Helicopter for Piloted Simulation,” NASA TM-84281, Sept. 1982.

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