New type-2-fuzzy-logic-based control system for the Cessna Citation X

SM Hosseini, G Ghazi, RM Botez - Journal of Aerospace Information …, 2024 - arc.aiaa.org
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 …

Comparison of optimal and bioinspired adaptive control laws for spacecraft sloshing dynamics

N Coulter, H Moncayo - Journal of Spacecraft and Rockets, 2020 - arc.aiaa.org
The presence of fuel slosh dynamics in a spacecraft system during a maneuver leads to
attitude control system (ACS) performance degradation resulting in attitude tracking errors …

A modified genetic algorithm for UAV trajectory tracking control laws optimization

B K. Wilburn, M G. Perhinschi… - International Journal of …, 2014 - emerald.com
Purpose–The purpose of this paper is to gain trajectory-tracking controllers for autonomous
aircraft are optimized using a modified evolutionary, or genetic algorithm (GA) …

Robust control architecture for wind rejection in quadrotors

J Verberne, H Moncayo - 2019 International Conference on …, 2019 - ieeexplore.ieee.org
Current efforts at the Advanced Dynamics and Control Laboratory (ADCL) at Embry-Riddle
Aeronautical University (ERAU) are focusing on the implementation of robust control laws for …

Enhanced fuzzy-based super-twisting sliding-mode control system for the Cessna Citation X Lateral Motion

SM Hosseini, I Bematol, G Ghazi, RM Botez - Aerospace, 2024 - espace2.etsmtl.ca
A novel combination of three control systems is presented in this paper: an adaptive control
system, a type-two fuzzy logic system, and a super-twisting sliding mode control (STSMC) …

A bio-inspired adaptive control compensation system for an aircraft outside bounds of nominal design

AE Perez, H Moncayo… - Journal of …, 2015 - asmedigitalcollection.asme.org
This paper presents a novel bio-inspired adaptive control technique that has been designed
to maintain the performance of an aircraft under upset conditions. The proposed control …

Virtual flight demonstration of the stratospheric dual-aircraft platform

WA Engblom, RK Decker - 34th AIAA Applied Aerodynamics …, 2016 - arc.aiaa.org
A baseline configuration for the dual-aircraft platform (DAP) concept is described and
evaluated in a physics-based flight dynamics simulations for two month-long missions as a …

Design of an attitude control system for a spacecraft with propellant slosh dynamics

N Coulter - 2018 - commons.erau.edu
The presence of propellant slosh dynamics in a spacecraft system during a maneuver leads
to attitude control system (ACS) performance degradation resulting in attitude tracking errors …

Development of Robust Control Laws for Disturbance Rejection in Rotorcraft UAVs

J Verberne - 2019 - commons.erau.edu
Inherent stability inside the flight envelope must be guaranteed in order to safely introduce
private and commercial UAV systems into the national airspace. The rejection of unknown …

Fault Tolerance Analysis of L1 Adaptive Control System for Unmanned Aerial Vehicles

K Krishnamoorthy - 2015 - researchrepository.wvu.edu
Trajectory tracking is a critical element for the better functionality of autonomous vehicles.
The main objective of this research study was to implement and analyze L1 adaptive control …