Aircraft Pitch Attitude Control using Backstepping
2000 (English)Report (Other academic)
A nonlinear approach to the automatic pitch attitude control problem for a generic fighter aircraft is presented. A nonlinear model describing the longitudinal equations of motion in strict feedback form is derived. Backstepping is utilized for the construction of a globally stabilizing controller with a number of free design parameters. Two tuning schemes are proposed based on the desired locally linear controller properties. The controller is evaluated using the HIRM fighter aircraft model.
Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 2000. , 13 p.
LiTH-ISY-R, ISSN 1400-3902 ; 2243
Nonlinear control, Aircraft control, Backstepping, Local approximation
IdentifiersURN: urn:nbn:se:liu:diva-55671ISRN: LiTH-ISY-R-2243OAI: oai:DiVA.org:liu-55671DiVA: diva2:316399