A novel estimation method for weight and center-of-gravity via the aircraft trim data-Reference-Cited by-同舟云学术

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A novel estimation method for weight and center-of-gravity via the aircraft trim data

Published:2023-10 Issue: Volume:220 Page:113362
ISSN:0263-2241
Container-title:Measurement
language:en
Short-container-title:Measurement

Author:

Zhai Shaobo,Li Guangwen,Huang Penghui,Hou Mingshan,Jia Qiuling

Funder

Shaanxi Key Laboratory of Flight Control and Simulation Technology

Publisher

Elsevier BV

Subject

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

Reference28 articles.

1. Particle filter for aircraft mass estimation and uncertainty modeling;Sun;Transport. Res. C-Emer.,2019

2. Preliminary development of an onboard weight and balance estimator for commercial aircraft;Chaves;Aerosp. Sci. Technol.,2018

3. Design and performance analyses of a fixed wing battery VTOL UAV;Dundar;Eng. Sci. Technol.,2020

4. A multi-scaled demonstrator for aircraft weight and balance measurements based on FBG sensors: Design rationale and experimental characterization;Brindisi;Measurement,2019

5. Extreme aircraft maneuver under sudden lateral CG movement: Modeling and control;Mukherjee;Aerosp. Sci. Technol.,2017

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