Metaheuristic-assisted complex H-infinity flight control tuning for the Hawkeye unmanned aerial vehicle: A comparative study
Selecting weighting factors for H-infinity controller requires tones of knowledge and
experience without guaranteeing obtaining the best results. This paper proposes novel idea …
experience without guaranteeing obtaining the best results. This paper proposes novel idea …
Review and comparison of clearance control strategies
B Gao, W Shen, H Guan, W Zhang, L Zheng - Machines, 2022 - mdpi.com
The nonlinearity of clearance has a significant influence on the performance of a system
while ensuring the reliability of the variable-speed transmission, and hinders the …
while ensuring the reliability of the variable-speed transmission, and hinders the …
A novel fault-tolerant air traffic management methodology using autoencoder and P2P blockchain consensus protocol
This paper presents a methodology for designing a highly reliable Air Traffic Management
and Control (ATMC) methodology using Neural Networks and Peer-to-Peer (P2P) …
and Control (ATMC) methodology using Neural Networks and Peer-to-Peer (P2P) …
Neural network adaptive controller with approximate dynamic inversion for pitch control of the Cessna Citation X
View Video Presentation: https://doi. org/10.2514/6.2023-3798. vid This paper presents a
technique for designing an adaptive nonlinear controller for the pitch rate of the Cessna …
technique for designing an adaptive nonlinear controller for the pitch rate of the Cessna …
Design of a Type Two Fuzzy-based system to Control the Pitch Rate of the Cessna Citation X
View Video Presentation: https://doi. org/10.2514/6.2023-3802. vid In this research, a novel
control methodology developed at the Laboratory of Applied Research in Active Controls …
control methodology developed at the Laboratory of Applied Research in Active Controls …
Stabilisation, tracking and disturbance rejection control design for the UAS-S45 Bálaam
The stabilisation and control mechanisms of an Unmanned Aerial System (UAS) must be
properly designed to ensure acceptable flight performance. During their operation, these …
properly designed to ensure acceptable flight performance. During their operation, these …
[PDF][PDF] New Methodology for Optimal Flight Control Using Differential Evolution Algorithms Applied on the Cessna Citation X Business Aircraft–Part 1. Design and …
Setting the appropriate controllers for aircraft stability and control augmentation systems are
complicated and time consuming tasks. As in the Linear Quadratic Regulator method gains …
complicated and time consuming tasks. As in the Linear Quadratic Regulator method gains …
New Type-2-Fuzzy-Logic-Based Control System for the Cessna Citation X
This paper presents a new control law based on type-2 fuzzy logic system (T2FLS) for the
Cessna Citation X aircraft during cruise. This methodology combines three control systems …
Cessna Citation X aircraft during cruise. This methodology combines three control systems …
Adaptive boundary sine cosine optimizer with population reduction for robustness analysis of finite time horizon systems
This paper proposes an adaptive boundary sine cosine optimizer with population reduction.
It is designed specifically to calculate an upper bound on the worst-case gain of a known …
It is designed specifically to calculate an upper bound on the worst-case gain of a known …
[PDF][PDF] New methodology for optimal flight control using differential evolution algorithms applied on the cessna citation x business aircraft–part 2. validation on aircraft …
In this paper the Cessna Citation X clearance criteria were evaluated for a new Flight
Controller. The Flight Control Law were optimized and designed for the Cessna Citation X …
Controller. The Flight Control Law were optimized and designed for the Cessna Citation X …