Automatic Pitch Control
Automatic Pitch Control is a flight control system—a subsystem of automatic flight control mechanisms—that regulates an aircraft's pitch attitude by automatically adjusting elevator or stabilizer positions to maintain or achieve desired longitudinal motion parameters without continuous pilot input.
26
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741
Citations
78
Authors
48
Institutions
Publications per year
2017–2026
6
Parents
26
Saber Abrazeh, A. Parvaresh, Saeid-Reza Mohseni et al. · IEEE/CAA Journal of Automatica Sinica · 2021 · 58 citations
Design of a new electrolarynx having a pitch control function
Norihiro Uemi, Tohru Ifukube, Masaharu Takahashi et al. · 2002 · 54 citations
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48

University of Helsinki
Helsinki, Finland
2 h-index
5 publications
262 citations

Consejo Nacional de Investigaciones Científicas y Técnicas
Buenos Aires, Argentina
1 h-index
1 publications
25 citations

Hokkaido University of Science
Sapporo, Japan
1 h-index
2 publications
108 citations

Ames Research Center
Mountain View, United States
1 h-index
3 publications
36 citations

TU Wien
Vienna, Austria
1 h-index
3 publications
105 citations
ETH Zurich
Zurich, Switzerland
1 h-index
2 publications
44 citations
General Dynamics (United States)
Reston, United States
1 h-index
1 publications
17 citations
Tokyo Institute of Technology
Tokyo, Japan
1 h-index
1 publications
11 citations
1–8 of 48
2 publications · 47 citations
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1 publications · 58 citations
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1 publications · 19 citations
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1 publications · 17 citations
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1 publications · 11 citations
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