Now showing items 1-2 of 2
Design of a flight stabilizer system and automatic control using HIL test platform
(International Journal Of Mechanical Engineering And Robotics Research, 2016)
In this paper a Hardware-In-the-Loop (HIL) test platform is used to design a flight stabilization system for Unmanned Aerial Vehicles (UAV). Controllers are first designed and tested separately for lateral and longitudinal ...
Robust Autopilot Design Based on a Disturbance/Uncertainty/Coupling Estimator
(Institute of Electrical and Electronics Engineers Inc., 2019-11)
Autopilot failures have caused fatal results for both military and civilian applications, leading to loss of life and property. Major contributing factors are disturbances (e.g., winds), uncertainties (e.g., unmodeled ...