We think you have liked this presentation. If you wish to download it, please recommend it to your friends in any social system. Share buttons are a little bit lower. Thank you!
Presentation is loading. Please wait.
Published byLincoln Halter
Modified about 1 year ago
Helicopter Hover Control VDM1-project F10 Lasse, Christian, Frederik
Since last time… Further requirements Initial class diagram 2
Further requirements Environment simulates change in position or angle to the respective sensor Environment is notified when system has reacted to change in environment 3
Initial class diagram 4
Level of abstraction Pitch and roll Rotor angle RPM 5
Next time Combined VDM++/UML model ? More extensive class diagram Start VDM++ modelling Further requirements 6
Helicopter Hover Control VDM1-project F10 Lasse, Christian, Frederik.
Scaled Helicopter Mathematical Model and Hovering Controller Brajtman Michal & Sharabani Yaki Supervisor : Dr. Rotstein Hector.
Radio Settings Curves 1 Sylvain Marron Modèle Air Club du Mâconnais Friday, March 4th 2011.
© 2009 Aviation Supplies & Academics, Inc. All Rights Reserved. Principles of Helicopter Flight Chapter 6 Aerodynamic Forces.
Settling with Power (vortex ring state) Front Range Helicopters.
Retreating Blade Stall Front Range Helicopters. Definition The stalled condition of the retreating blade when it operates beyond its critical (stall)
Aerodynamics FF-1/01 Aero Foundations Translating Tendency Ground Effect Translational Lift Transverse Flow Dissymmetry of Lift Drag Total Aerodynamic.
© 2009 Aviation Supplies & Academics, Inc. All Rights Reserved. Principles of Helicopter Flight Chapter 20 Helicopter Design and Components.
SPECIAL RIGHT TRIANGLES Lesson º-60º-90º Triangles Theorem 72: In a triangle whose angles have the measures of 30 º, 60 º, and 90 º, the lengths.
NONLINEAR BACKSTEPPING CONTROL WITH OBSERVER DESIGN FOR A 4 ROTORS HELICOPTER L. Mederreg, F. Diaz and N. K. M’sirdi LRV Laboratoire de Robotique de Versailles,
Shapes and Angle Rules 80 + ? = = 180.
Angles and parallel lines a° b° Corresponding angles for parallel lines are equal m n t m and n are parallel lines, t is a Transversal A transversal is.
Richard Shepherd - Jose Rios - Bruk Sahilu. Mission: Team Airwolf is set to test the stresses applied to a Helicopter Rotor Blade as it rotates about.
Our acceleration prediction model Predict accelerations: f : learned from data. Obtain velocity, angular rates, position and orientation from numerical.
Automobile Charging System By Daniel Joo Functional Diagram Alternator Signal Conditioning Voltage Regulation.
Helicopters How a helicopter is able to fly Click anywhere to Launch.
Presented by:- Suman Kumar. INTRODUCTION : Quad-rotor helicopters are emerging as a popular unmanned aerial vehicle configuration because of their simple.
1 An open belt drive transmits power through a pulley having a diameter of 300 mm at a speed of 150 rpm. The belt is 10 mm thick and 150 mm wide and has.
Date of download: 7/8/2016 Copyright © ASME. All rights reserved. From: A Mobile Motion Capture System Based on Inertial Sensors and Smart Shoes J. Dyn.
Where: I T = moment of inertia of turbine rotor. T = angular shaft speed. T E = mechanical torque necessary to turn the generator. T A = aerodynamic.
Model-View-Controller A Design Pattern SE-2030 Dr. Rob Hasker 1 Based on slides written by Dr. Mark L. Hornick Used with permission.
Qball-X4 Simulator Seang Cau February 16, Introduction Simulator is run under MatLAB and rendered using Quarc. Simulates the behavioral properties.
II Explanation of the Electric Motor Demonstrated in Class.
Principles of Flight Chapter 6 – Helicopters. Introduction A helicopter generates both lift and thrust by using its rotor blades rather than wings. Blades.
6.111 Final Project A motion sensor baseball game By Chris Falling and JinHock Ong.
EC 130 B4 Initial Pilot Ground School Chapter 6 Tail Rotor Drive System and Tail Rotor.
SD-May1014 Team: Michael Peat, Kollin Moore, Matt Rich, Alex Reifert Advisors: Dr. Nicola Elia and Dr. Phillip Jones.
UML Diagrams: Use Case Diagrams Prof. Hany Ammar, CSEE Dept., WVU.
Application of UML for Hardware Design Based on Design Process Model By Robertas Damasevicius, Vytautas Stuikys Presented by Matt Roth.
Section Law of Sines and Area SAS Area 1-90 Since SAS determines a triangle, it should be possible to find its area given the 2 sides and the angle.
Round and Round They Go. Helicopter helicopter – a plane that gets its lift from a powered rotor.
August Two courses on VDM++ for Embedded Systems: Learning by Doing Professor Peter Gorm Larsen Engineering College of Aarhus Computer Technology.
Torque Reaction The fuselage’s reaction to the turning of the main rotor system is Torque Reaction The fuselage’s reaction to the turning of the main rotor.
Find the angle between the forces shown if they are in equilibrium.
Edexcel A2 Physics Unit 4 : Chapter 1.2 : Motion In a Circle Prepared By: Shakil Raiman.
Physics 101: Lecture 13, Pg 1 Physics 101: Lecture 13 Rotational Kinetic Energy and Inertia Exam II.
3.5 Parallel Lines and Triangles Parallel Postulate –Through a point not on a line, there is one and only one line parallel to the given line.
Composite 3D Transformations. Example of Composite 3D Transformations Try to transform the line segments P 1 P 2 and P 1 P 3 from their start position.
Use Case Modeling Chapter 7 Part of Requirements Modeling Designing Concurrent, Distributed, and Real-Time Applications with UML Hassan Gomaa (2001)
SIMULATION OF 2-DOF HELICOPTER RESULTS Maryam Alizadeh June 29 th
Flight Simulator X By Dane Wrye, Aaron Pena, and Ben Ghusn.
Whiteboardmaths.com © 2004 All rights reserved
The Helicopter. How do Helicopters Fly Helicopters generate lift by rotating its wings!! A cross-section of a rotor blade has an aerofoil shape, similar.
Date of download: 6/27/2016 Copyright © ASME. All rights reserved. From: Magnetic Bearing Rotordynamic System Optimization Using Multi-Objective Genetic.
A Position Detection Strategy for Sensorless Surface Mounted Permanent Magnet Motors at Low Speed Using Transient Finite-Element Analysis Zhao Wang, Shuangxia.
TECHNOLOGY DEMONSTRATOR OF 7-CHANNEL DIGITAL FLIGHT DATA RECORDER AS AVIONICS TEACHING AID USING STATIC MODEL AIRCRAFT Authors 1. Wg Cdr Nikhil Verma,
UML Activity Diagram. Activity Diagram The main reason to use activity diagrams is to model the workflow behind the system being designed. Activity.
HELICOPTER AERODYNAMICS. BASIC DEFINITIONS Shaft Axis The shaft axis is the axis of the main rotor shaft and about which the blades are permitted to rotate.
THE POWER OF THE WIND. The wind: a key factor in world economy Wind needs clean, renewable and competitive sources of energy; wind is a very competitive.
© 2017 SlidePlayer.com Inc. All rights reserved.