A5009081609- AI in Service Interactions
- Social Robot Interaction and HRI
- Robotics and Automated Systems
- Cavitation Phenomena in Pumps
- Robotics and Sensor-Based Localization
- Advanced Aircraft Design and Technologies
- Underwater Vehicles and Communication Systems
- Guidance and Control Systems
- Target Tracking and Data Fusion in Sensor Networks
- Aerospace Engineering and Control Systems
- Inertial Sensor and Navigation
- Rocket and propulsion systems research
- Advanced Multi-Objective Optimization Algorithms
- Mechanical Engineering and Vibrations Research
Instituto Politécnico Nacional
2016-2018
Centre National de la Recherche Scientifique
2017
Laboratoire d'Analyse et d'Architecture des Systèmes
2017
Tecnológico Nacional de México
2017
Université de Toulouse
2017
An optimization problem based on discrete-integer and continuous variables in order to design a multirotor for specific application (maximum thrust-to-weight maximum flight time) is developed. We considered the length diameter of rods as selection motors, propellers, battery variables, components selected are available common hobby stores. The solved two cases: ratio time. stated using aerodynamic principles mechanical well. used Genetic Algorithm provided by Optimization Toolbox Matlab®,...
This paper proposes a new mathematical model to map the rotational speed and angle of attack (pitch) small-size propellers typically used in multirotors aerodynamic thrust force drag moment produced by propeller itself. The is inspired standard models using blade-element momentum theories, which have been suitably modified order allow for explicit fast computation direct inverse (useful high-frequency control) obtain better adherence experimental data. allows captures all main nonlinear...
This paper presents the description and experimental results of a versatile Visual Marker based Multi-Sensor Fusion State Estimation that allows to combine variable optional number sensors positioning algorithms in loosely-coupling fashion, incorporating visual markers increase its performances. technique an aerial robot navigate different environments carrying out missions with same state estimation architecture, exploiting best from every sensor. The algorithm has been successfully tested...
In this paper, a methodology to design hexa-rotor with the capability reject disturbances using tilted propellers is presented. The proposes use of robustness index as measurement external disturbances. Moreover, an energy proposed consumed by in hovering. It shown that opposed index. Therefore, multi-objective optimization problem which objective functions are and This solved help evolutionary algorithm Pareto approach. Three solutions selected from front tested controller order show...