LOW-SPEED TURNING FLIGHT PATH CONTROL OF A STOL AIRCRAFT

Authors
KANNO S KAMIMURA M OHTA H CHUBACHI T
Citation
S. Kanno et al., LOW-SPEED TURNING FLIGHT PATH CONTROL OF A STOL AIRCRAFT, Transactions of the Japan Society for Aeronautical and Space Sciences, 38(119), 1995, pp. 16-37
Citations number
NO
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
Transactions of the Japan Society for Aeronautical and Space Sciences → ACNP
ISSN journal
05493811
Volume
38
Issue
119
Year of publication
1995
Pages
16 - 37
Database
ISI
SICI code
0549-3811(1995)38:119<16:LTFPCO>2.0.ZU;2-K
Abstract
This paper is concerned with an automatic low speed turning flight pat h control system design for a STOL aircraft. A right control system is designed using an approximate perfect servo, which is effective to th e control of non-minimum phase plant. A complementary input method whi ch will reduce the control errors of this servo system is introduced. Favourable simulation results are obtained which will substantiate the effectiveness of present methods.