Longitudinal Stability Analysis of STTA-12 MXA

DOI

10.2991/978-94-6463-358-0_22How to use a DOI?

Keywords

stability; longitudinal; STTA-12MXA

Abstract

This paper present the result of simulation longitudinal stability on STTA-12 MXA aircraft. This aircraft is included in the utility aircraft category with 1 propeller engine and 2 seats. The longitudinal response mode has been determined. The Datcom program is used to estimate the parameters in the longitudinal derivatives. As the next step, the longitudinal motion of aircraft is simulated and the transfer functions of linearized equations of motion have been obtained. The Phugoid and short period modes have been investigated. The damping and frequency of both the phugoid and short period influence the handling or flying qualities of an airplane.

Copyright

© 2023 The Author(s)

Open Access

Open Access This chapter is licensed under the terms of the Creative Commons Attribution-NonCommercial 4.0 International License (http://creativecommons.org/licenses/by-nc/4.0/), which permits any noncommercial use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license and indicate if changes were made.

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TY  - CONF
AU  - Bangga Dirgantara Adiputra
AU  - Okto Dinaryanto
AU  - buyung Junaidin
AU  - Lazuardy Pinandhita
PY  - 2024
DA  - 2024/01/12
TI  - Longitudinal Stability Analysis of STTA-12 MXA
BT  - Proceedings of the 2023 Annual Technology, Applied Science and Engineering Conference (ATASEC 2023)
PB  - Atlantis Press
SP  - 221
EP  - 228
SN  - 2352-5401
UR  - https://doi.org/10.2991/978-94-6463-358-0_22
DO  - 10.2991/978-94-6463-358-0_22
ID  - Adiputra2024
ER  -