Automatic carrier landing system based on active disturbance rejection control with a novel parameters optimizer

Y Yu, H Wang, N Li, Z Su, J Wu - Aerospace science and technology, 2017 - Elsevier
This paper proposes an active disturbance rejection control (ADRC) scheme for automatic
carrier landing system (ACLS) in final approach. To track desired touchdown point (DTP) …

Optimal satellite formation reconfiguration based on closed-loop brain storm optimization

C Sun, H Duan, Y Shi - IEEE Computational Intelligence …, 2013 - ieeexplore.ieee.org
In recent years, satellite formation flying has become an increasingly hot topic for both the
astronomy and earth science communities due to its potential merits compared with a single …

Control parameter design for automatic carrier landing system via pigeon-inspired optimization

Y Deng, H Duan - Nonlinear Dynamics, 2016 - Springer
In this paper, a novel control parameter design method is presented for the automatic carrier
landing system. To overcome difficulties in the manual parameter adjustment task, the …

Simplified brain storm optimization approach to control parameter optimization in F/A-18 automatic carrier landing system

J Li, H Duan - Aerospace science and Technology, 2015 - Elsevier
The design of automatic carrier landing system is a crucial technique for carrier-based
aircraft, since it facilitates landing of aircraft on carriers in various severe weather conditions …

Multi-objective pigeon-inspired optimization for brushless direct current motor parameter design

HX Qiu, HB Duan - Science China Technological Sciences, 2015 - Springer
Pigeon-inspired optimization (PIO) is a new swarm intelligence optimization algorithm,
which is inspired by the behavior of homing pigeons. A variant of pigeon-inspired …

Comprehensive Review of Metaheuristic Algorithms (MAs) for Optimal Control (OCl) Improvement

U Mohammed, T Karataev, O Oshiga… - … Methods in Engineering, 2024 - Springer
Optimal control (OCl) can be traced back to the 1960s when it was utilised for solving an
optimisation problem (OP). In the OCl technique, a stable controller can be obtained by …

Composite observer-based robust model predictive control technique for ducted fan aerial vehicles

T Manzoor, H Pei, Z Cheng - Nonlinear Dynamics, 2023 - Springer
The ducted fan aircraft are an important type of hybrid aerial vehicle due to their annular
safety mechanism called duct. Despite their numerous advantages, developing a control …

[PDF][PDF] Optimal tuning of linear quadratic regulators using quantum particle swarm optimization

K Hassani, WS Lee - Proceedings of the International Conference on …, 2014 - avestia.com
Linear Quadratic Regulator (LQR) is an optimal multivariable feedback control approach that
minimizes the excursion in state trajectories of a system while requiring minimum controller …

Finite-time model-assisted active disturbance rejection control with a novel parameters optimizer for hypersonic reentry vehicle subject to multiple disturbances

Y Yu, H Wang, N Li, H Zhang, Z Su, X Shao - Aerospace Science and …, 2018 - Elsevier
In this paper, a scheme which combines finite-time model-assisted active disturbance
rejection control and novel greedy criterion-based salp swarm algorithm is developed for …

Trophallaxis network control approach to formation flight of multiple unmanned aerial vehicles

HB Duan, QN Luo, YX Yu - Science China Technological Sciences, 2013 - Springer
A novel network control method based on trophallaxis mechanism is applied to the formation
flight problem for multiple unmanned aerial vehicles (UAVs). Firstly, the multiple UAVs …