Journal of System Simulation
Abstract
Abstract: The frame and characteristic of self-adaptive flight control system with self-repair function for aircraft with thrust vector were studied. RHO optimal algorithm was used to realize online controller design. MSLS algorithm was used to realize online flight identify parameters. Global parity space method, sensor data fusion and probability theory were used to realize FDI algorithm. The simulation platform used to simulate self-repair function with aircraft control surface failure was developed using OOP language VC++6.0 and three-dimensional graphics language OpenGL. Simulations show that the control surface and flight aerodynamic parameter change with flying states in the flight movement simulation. In this platform, the faults of the flight can be loaded to the flight system according to user’s need, and has fine self-repair function.
Recommended Citation
Hao, Long and Song, Shujie
(2020)
"Study of Setting up Simulation Platform of Self-adaptive Flight Control System with Self-repair Function,"
Journal of System Simulation: Vol. 27:
Iss.
11, Article 24.
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol27/iss11/24
First Page
2791
Revised Date
2014-03-28
DOI Link
https://doi.org/
Last Page
2796
CLC
G590.6510
Recommended Citation
Long Hao, Song Shujie. Study of Setting up Simulation Platform of Self-adaptive Flight Control System with Self-repair Function[J]. Journal of System Simulation, 2015, 27(11): 2791-2796.
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