Aircraft pitch and heave rate control

Authors
Whalley, R Ebrahimi, RI
Citation
R. Whalley et Ri. Ebrahimi, Aircraft pitch and heave rate control, P I MEC E G, 214(G1), 2000, pp. 1-8
Citations number
13
Categorie Soggetti
Aereospace Engineering
Journal title
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
ISSN journal
09544100 → ACNP
Volume
214
Issue
G1
Year of publication
2000
Pages
1 - 8
Database
ISI
SICI code
0954-4100(2000)214:G1<1:APAHRC>2.0.ZU;2-M
Abstract
The dynamic model of a high-performance military aircraft is considered. An input-output representation relating the open-loop pitch and heave rate ch aracteristics to elevator movement is derived. Effective closed-loop design techniques are invoked. Simulated response transients are presented.