0000000000710223

AUTHOR

Krishneel Kumar

0000-0002-9449-0244

showing 3 related works from this author

Robust motion control of nonlinear quadrotor model with wind disturbance observer

2021

This paper focuses on robust wind disturbance rejection for nonlinear quadrotor models. By leveraging on nonlinear unknown observer theory, it proposes a nonlinear dynamic filter that, using sensors already on-board the aircraft, can estimate in real-time wind gust signals in the three dimensions. The wind disturbance is then treated as input to the PD controller for a quick and robust flight pathway in presence of disturbances. With this scheme, the wind disturbance can be precisely estimated online and compensated in real-time. Hence, the quadrotor can successfully reach its desired attitude and position. To show the effective and desired performance of the method, simulation results are …

General Computer ScienceObserver (quantum physics)PD controlComputer scienceGeneral EngineeringPID controllerNonlinear unknown input observersFilter (signal processing)Motion controlUnknown wind gust estimation and compensationTK1-9971Nonlinear systemControl theoryRobustness (computer science)QuadrotorGeneral Materials ScienceNonlinear unknown input observers; PD control; Quadrotor; Unknown wind gust estimation and compensationElectrical engineering. Electronics. Nuclear engineeringRobust controlMATLABcomputercomputer.programming_language
researchProduct

Wind gust estimation for precise quasi-hovering control of quadrotor aircraft

2021

Abstract This paper focuses on the control of quadrotor vehicles without wind sensors that are required to accurately track low-speed trajectories in the presence of moderate yet unknown wind gusts. By modeling the wind disturbance as exogenous inputs, and assuming that compensation of its effects can be achieved through quasi-static vehicle motions, this paper proposes an innovative estimation and control scheme comprising a linear dynamic filter for the estimation of such unknown inputs and requiring only position and attitude information. The filter is built upon results from Unknown Input Observer theory and allows estimation of wind and vehicle state without measurement of the wind its…

QuadcopterUnknown Input-state observersOffset (computer science)Observer (quantum physics)Computer scienceRotor (electric)Applied MathematicsRobust controlRoboticsROS/GazeboComputer Science Applicationslaw.inventionCompensation (engineering)Tracking errorQuadrotorsControl and Systems EngineeringControl theoryPosition (vector)Filter (video)lawDisturbance observersElectrical and Electronic EngineeringDisturbance observers; Quadrotors; Robotics; Robust control; ROS/Gazebo; Unknown Input-state observers
researchProduct

Erle-copter Simulation using ROS and Gazebo

2020

The recent decrease in the price as well as size of semi-conductor logic and due to significant advancements in technologies such as microcontrollers, motors and sensors, the application of quadcopters in several fields has been achieved. However, testing of quadcopter prototypes still has a risk of damage due to faults and unexpected behavior. Hence, a method of testing of quadcopters in simulation mimicking the actual conditions of the real environment in an actual hardware test has been proposed. For this purpose, Gazebo simulator integrated with ROS has been chosen for the simulation of the path of the quadcopter. Moreover, the software Matlab/Simulink has been interfaced with Gazebo in…

QuadcopterROS; Gazebo; UAV; GCS; autonomous vehicle; simulation; Erle-copterComputer sciencebusiness.industryUAVautonomous vehicleErle-copterROS Gazebo UAV GCS autonomous vehicle simulation Erle-copter.ROSGCSsimulationMicrocontrollerSoftwareSettore ING-INF/04 - AutomaticaGazeboMATLABbusinesscomputerSimulationcomputer.programming_language
researchProduct