Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
- Authors: Petunin V.I.1, Neugodnikova L.M.1
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Affiliations:
- Ufa State Technical University
- Issue: Vol 62, No 1 (2019)
- Pages: 32-41
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230815
- DOI: https://doi.org/10.3103/S1068799819010057
- ID: 230815
Cite item
Abstract
The problem on restriction of aircraft motion parameters is considered. Features of constructing the logical dynamic systems of critical parameters restriction for different channels of aircraft angular motion control are shown. The problems of synthesizing such systems are considered. The simulation results are presented.
About the authors
V. I. Petunin
Ufa State Technical University
Author for correspondence.
Email: petunin_vi@mail.ru
Russian Federation, ul. K. Marksa 12, Ufa, Bashkortostan, 450000
L. M. Neugodnikova
Ufa State Technical University
Email: petunin_vi@mail.ru
Russian Federation, ul. K. Marksa 12, Ufa, Bashkortostan, 450000