Design & Development of a Quad Rotor MAV Beniamin Apopei

Slides:

Advertisements

Similar presentations

System Simulation made easy by. Efficient Simulator Technology - Several analysis types / initialization options - Coupled analogue and digital simulators.

Advertisements

Georgia Tech Aerial Robotics Dr. Daniel P Schrage Jeong Hur Fidencio Tapia Suresh K Kannan SUCCEED Poster Session 6 March 1997.

System Simulation made easy by. Multi-Physics System Simulator Electrical Electronics, power electronics, rotating machines, spice semiconductors… Mechanics.

System Simulation made easy by Electric Circuits Electronics, Power Electronics, Machines, Semiconductors... Thermal Networks Conduction, Convection,

Nonlinear Control of Quadrotor

Torque Reaction The fuselage’s reaction to the turning of the main rotor system is Torque Reaction Newton's third law of motion states that for every action,

Team Shane Stumvoll, Alex Willard, Robert Yarnell, Hubert Jayakumar, Tim Teal 1.

The Helicopter.

David Gitz, EE, ICARUS Lead Engineer Senior Design.

Helicopter Hover Control VDM1-project F10 Lasse, Christian, Frederik.

Outline quad-copter Abstract Quad-Copter Movement Hand movement

Pima Community College 4/12/14 Team Members Nick Patzke Gustavo Guerrero Nick Morris UAV Design, Manufacture and Applications Arizona NASA Space Grant.

2E1242 Project Course Automatic Control - The Helicopter.

Scaled Helicopter Mathematical Model and Hovering Controller Brajtman Michal & Sharabani Yaki Supervisor : Dr. Rotstein Hector.

SD-May1014 Team: Michael Peat, Kollin Moore, Matt Rich, Alex Reifert Advisors: Dr. Nicola Elia and Dr. Phillip Jones.

Boy Scouts Aviation Merit Badge Control Surfaces.

Autonomous Quadrocopter Proposal Brad Bergerhouse, Nelson Gaske, Austin Wenzel Dr. Malinowski.

A.U.V. Emeric Rochford Dale Williams Bryan Douse Ryan Gray.

M OBILE D EFENSE SYSTEM WITH AUGMENTED AIR ROVER Project Adviser: Dr. Muhammad Tahir Group Members: Adnan Chaudhary (2009-EE-103) Zeeshan Mahmood (2009-EE-108)

Midterm review 2E1242 – Automatic Control Helicopter Project.

AAE450 Spring 2009 Hopper Trajectory February 26, 2009 [Alex Whiteman] [Mission Ops] [Lunar Descent] Page 1.

E- 579 Mechatronics Modeling and Simulation Term Project - “ Steer By Wire” Instructor Dr. Shuvra Das Divesh Mittal.

EDGE™ MAV Control System - P Management Review (MSD I) Erik Bellandi – Project Manager Ben Wager – Lead Engineer Garrett Argenna – Mechanical Engineering.

Propulsion PDR #2 Brian Barnett Rob Benner Ryan Srogi John Keune Alex Fleck.

Robotic Arm Controller A VLSI Implementation Team: Justin Hamann & Dave McNamara Team: Justin Hamann & Dave McNamara Advisor: Dr. Vinod Prasad Advisor:

Barry Barrios Structural Engineer Daniel Chaparro Structural Engineer Laura Garrity Propulsion Chad Lieberman Control Surfaces Adam Vaccaro Electrical.

Vehicle Tracking/Payload Release System For Small UAV Project Team

EDGE™ MAV Control System - P09122 Final Project Review Erik Bellandi – Project Manager Ben Wager – Lead Engineer Garrett Argenna – Mechanical Engineering.

Digital Art is Interactive Visual Art. How has art been changed because of technology ?

Quadcopters. History Also known as quadrotors First flying quadrotor: – 11 November 1922 – Etienne Oehmichen Image: blogger.com.

Kick off meeting, swarm E2E study, nio #1 8-Sep-15 Development Approach Task 1: Industrial Module –to be used by industry for their system simulation –Output:

Development of a Mini-UAV for Urban Environments Tony Dodd and Beniamin Apopei.

David Gitz, EE, ICARUS Lead Engineer Senior Design.

Rotorcraft Handling Qualities and System Identification

SPUD TC (OCT 07) REVISION ACADEMICS. SPUD TASK 1114 PERFORM A ROLLING TAKEOFF.

Disturbance Rejection: Final Presentation Group 2: Nick Fronzo Phil Gaudet Sean Senical Justin Turnier.

Status Report #2 Automatic Child Safety Gate: Corry Winslow Roger Battles Philip So Description: A telescoping gate with sensor technology through the.

Whitman and Atkeson.  Present a decoupled controller for a simulated three-dimensional biped.  Dynamics broke down into multiple subsystems that are.

T L = 0.5 Fig. 6. dq-axis stator voltage of mathematical model. Three Phase Induction Motor Dynamic Modeling and Behavior Estimation Lauren Atwell 1, Jing.

David Gitz, EE, ICARUS Lead Engineer.  Michael Welling  PhD Candidate  ICARUS Vehicle Engineer  Ben Wasson  Masters Student  ICARUS Business Manager.

Towards Establishing and Maintaining Autonomous Quadrotor Formations Audrow J. Nash William Lee College of Engineering University of North Carolina at.

Students: Chen-Jay Xu Zheng-Xian Hung Advisor: Ru-Li Lin.

Presented by:- Suman Kumar. INTRODUCTION : Quad-rotor helicopters are emerging as a popular unmanned aerial vehicle configuration because of their simple.

Weight and Balance.

ITU LCH Structural Design Criteria and Structure Analysis March 19, 2003.

UPDATE #2.  The predicted altitude was ~9500 feet.  Actual altitude was ~11960 feet.  After investigation the error was found in the simulated weight.

By: Stuti Vyas( ) Drashti Sheth( ) Jay Vala( ) Internal Guide Mr. J. N. Patel.

Camera. “Up”, “Forward” and “Along” The three camera view vectors are defined as shown:

Quad copter Progress Report II October 15 – October 29 Team 22 Shawn Havener Mehdi Hatim.

Minor Project on Vertical Take-off Landing System SUBMITTED BY:- SHUBHAM SHARMA ( ) ABHISHEK ARORA ( ) VIBHANSHU JAIN ( )

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS)

P07122: Autonomous Quadcopter Jason Enslin – EE: Team Leader, Circuit Design/Testing Glenn Kitchell – CE: Programming, Software Design Richard Nichols.

Private Pilot Ground School

SAE Aero 2017 Midterm Presentation Joe Zongolowicz, Nick Montana, Frank Dixon, Kevin Scheventer, Kathy Hansen, Marquis Ward, Gerald Short, Zhangsiwen Xiao,

DYNAMICS & CONTROL PDR 1 TEAM 4

Sérgio Ronaldo Barros dos Santos Cairo Lúcio Nascimento Júnior

Propulsion QDR 2 Team #3 Presented by: Greg Davidson Etan Karni.

2018 First Nation Launch - Flight Readiness Review

QUANSER Flight Control Systems Design 2DOF Helicopter 3DOF Helicopter 3DOF Hover 3DOF Gyroscope Quanser Education Solutions Powered by.

Physics-based simulation for visual computing applications

RIT Space Exploration Group (SPEX)

Flight Controller and Ground Station Software

2019 First Nation Launch – PDR Virtual Review

P07122: Autonomous Quadcopter

Command and Data Handling

Chapter 1. Introduction to Control System

<Your Team # > Your Team Name Here

2019 First Nation Launch – Oral Presentation

Presentation transcript:

Design & Development of a Quad Rotor MAV Beniamin Apopei Quattro Copter Design & Development of a Quad Rotor MAV Beniamin Apopei 14/09/2005

General Description Goals: Achievements: Vertical Take off and Landing MAV Stable and Maneuverable Flight Time >10 min Minimum Payload: 250g As small as possible Design, construction, matlab simulation and control Achievements: 4 propellers MAV, 6 DOF Physical and Mathematic modelling. Matlab simulation Visual Interface for Control and Monitoring Take off, stable hovering and landing

Why 4 propellers? Problems: Coupled inputs Complicated rotor mechanics Watts / Weight Efficiency Reaction Torque

4 Propellers Model

Mathematic Model States Vector System Function System Inputs

Sistem’s Stability Subsystem Operating Point Liapunov Function [1] [2] We choose inputs [3] Results [4]

Inputs Correlation Altitude Variation as a result of Roll/ Pitch andYaw

Matlab Simulation Model Simulation diagram

Visual Interface

Final Model

First Experiments Stability Noise problems Brushed Motors A/D &Digital together Serial Com Software Personal Satisfaction Research Proposal