Estimation of aircraft centre of gravity using Kalman filters

Andrew Stanley, Roger Goodall

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

The centre of gravity (cg) of an aircraft is of fundamental importance to its stability, but it is difficult to measure precisely in-flight because it will vary as the aircraft manouevres and fuel is consumed and sloshes in its tanks. This paper describes the development of a longitudinal cg estimator using Kalman filters. Two examples are provided of the estimator. The first example uses a linear Phantom F4-C aircraft model in which an unexpected moment representing a cg change is injected into the aircraft and then estimated, and the second example uses a linearised version of a more comprehensive aircraft model, ADMIRE.

Original languageEnglish
Title of host publication2009 European Control Conference
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1848-1853
Number of pages6
ISBN (Print)9783952417393
DOIs
Publication statusPublished - 2009
Externally publishedYes
Event10th European Control Conference - Budapest, Hungary
Duration: 23 Aug 200926 Aug 2009
Conference number: 10

Conference

Conference10th European Control Conference
Abbreviated titleECC 2009
CountryHungary
CityBudapest
Period23/08/0926/08/09

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Stanley, A., & Goodall, R. (2009). Estimation of aircraft centre of gravity using Kalman filters. In 2009 European Control Conference (pp. 1848-1853). [7074672] Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.23919/ECC.2009.7074672