X-Pilot: Autopilot Solutions C. Edwards, J. Lasseigne, W. Overstreet, B. Penland Project Description: The X-Pilot: Autopilot Solutions project is developing.

Slides:



Advertisements
Similar presentations
1 DWC FLIGHT TEST EDUCATION AT UNDERGRADUATE LEVEL IN REALIZATION OF CDIO INITIATIVES 2009 International CDIO Conference June 7-10, 2009 Singapore Polytechnic.
Advertisements

By: Evan Olson and Vishal Doshi. Introduction Autonomous Vehicles allow expanded capabilities over manned data collection Relatively low cost, versatile.
MicroCART Micro processor C ontrolled A erial R obotics T eam Abstract MicroCART is a group of EE/CprE students tasked with developing an autonomous helicopter.
Design Presentation Spring 2009 Andrew Erdman Chris Sande Taoran Li.
Autonomous Sensor and Control Platform Rover Tae Lee Josh Reitsema Scott Zhong Mike Chao Mark Winter.
Seismic Octave Programming for Analog/Digital Converters Michael W. Siekman Electrical and Computer Engineering Senior Capstone Design Project 2007 Advisor:
SD-May1014 Team: Michael Peat, Kollin Moore, Matt Rich, Alex Reifert Advisors: Dr. Nicola Elia and Dr. Phillip Jones.
Autonomous Quadrocopter Proposal Brad Bergerhouse, Nelson Gaske, Austin Wenzel Dr. Malinowski.
MASKS © 2004 Invitation to 3D vision Lecture 11 Vision-based Landing of an Unmanned Air Vehicle.
Networked HVAC Controller Bradley University Department of Electrical & Computer Engineering By: Ed Siok Advisor: Dr. Malinowski.
Field Navigational GPS Robot Final Presentation & Review Chris Foley, Kris Horn, Richard Neil Pittman, Michael Willis.
Mars Rover TEAM CPNE Crossen Davis Peter Ramer Nancy Robinson Eric Rodriguez.
Camera Control Group Members - Bryan Marek - Brendan McMeel - Caitlin Motsinger - Tanya Ngo - Chris Hippleheuser.
Autonomous Dual Navigation System Vehicle Dmitriy Bekker Sergei Kunsevich Computer Engineering Rochester Institute of Technology December 1, 2005 Advisor:
University of Massachusetts Amherst InteLock TM Team: Emmanuel Seguin Josh Coffin Anh-Kiet Huynh Christos Tsiokos Remote Access and Proximity Key Advisor:
1 Practical Exercise Autonomous Aerial Search Vehicle (AASV)
EDGE™ MAV Control System - P09122 Final Project Review Erik Bellandi – Project Manager Ben Wager – Lead Engineer Garrett Argenna – Mechanical Engineering.
Aircraft Response to Control Input Data Collection System Presenter: Curtis Cutright Advisor: Dr. Michael Braasch Project Sponsor: JUP.
Client: Space Systems & Controls Laboratory (SSCL) Advisor : Matthew Nelson Anders Nelson (EE) Mathew Wymore (CprE)
Μ - CART Microprocessor – Controlled Aerial Robotics Team (Ongo03) An Ongoing Senior Design Project Department of Electrical and Computer Engineering Iowa.
Team Phoenix March 15, Project Goal Our team will develop an air vehicle that will not only navigate a course autonomously while providing real.
Intelligent Vehicles and Systems Group The Pennsylvania State University 1/9 EDSGN 100 EDSGN 100 Autonomous System Navigation and Driver Augmentation Pramod.
Unmanned aerial systems, what they are and what is available? Professor Sandor M Veres University of Sheffield.
How cheap and simple can a UAV be? Chris Anderson, Wired Magazine/DIY Drones.
1.  The Autonomous Helicopter Navigation System 2010 is focused on developing a helicopter system capable of autonomous control, navigation and localising.
Vision-based Landing of an Unmanned Air Vehicle
Wandering Ambassador P13215 Baabak Mamaghani (EE) Team Lead David Gillette (EE) PCB Matt Pendel (EE) PCB/Enclosure Armando Briones (CE) Software Sagar.
ECE415 Senior Design Project Spring 2009 FPR Presentation Robert Basile Rowan Oberski Qiaowen Zheng Danxiang Li Faculty Advisor: Russell Tessier Enjoy.
Hardware Overview Autopilot Control Board- Serves as common platform for other components and has autopilot code and flight plans Battery- Powers the.
Introduction UAV is an Unmanned Aerial Vehicle Our goal is to setup two different plane configurations with Paparazzi autopilot and fly them autonomously.
COBXXXX EXPERIMENTAL FRAMEWORK FOR EVALUATION OF GUIDANCE AND CONTROL ALGORITHMS FOR UAVS Sérgio Ronaldo Barros dos Santos,
Design Team # 4 Design of low cost flight computer for unmanned aerial vehicles Status Report # 4 Ryan Morlino Chris Landeros Sylvester Meighan Stephen.
By: Eric Backman Advisor: Dr. Malinowski.  Introduction  Goals  Project Overview and Changes  Work Completed  Updated Schedule.
Hardware Overview Autopilot Control Board- Serves as common platform for other components and has autopilot code and flight plans Battery- Powers the board.
Network UAV C3 Stage 1 Final Briefing Timothy X Brown University of Colorado at Boulder Interdisciplinary Telecommunications Program Electrical and Computer.
Small, Lightweight Speed and Distance Sensor for Skiers and Snowboarders Michael Bekkala Michael Blair Michael Carpenter Matthew Guibord Abhinav Parvataneni.
Michael Lisoski Leblanc Meneses Jason Schaer Bryan Staton.
Network Enabled Wearable Sensors The Combined Research Curriculum Development (CRCD) project works with the Virtual Reality Applications Center (VRAC)
Aerospace Digital Communication Instrument Senior Design 1 Presentation.
Mid-Semester Presentation Senior Design October 5, 2010
Senior Design II, Mid-semester Presentation October 5, 2010.
Powerpoint Templates Page Senior Design II Mid-Semester Presentation.
Mountain Bike Rallying SDII Mid-Term Presentation September 30, 2008.
Path The purpose of this project is to design a universal data recording device to monitor the health of a Dresser-Rand compressor during operation. In.
Aerospace Digital Communication Instrument Senior Design Presentation.
Mid – Semester Presentation Senior Design February 18, 2010.
Dual-Use Wideband Microphone System
Mid – Semester Presentation Senior Design February 25, 2010.
Smoke Notification System (SNS) Final Presentation Senior Design II November 19, 2013.
Advisor: Zhao Zhang Team Members: Chris Chambers Christopher Reis Alex Dean Luke Breuer SPALDING GYMNASTICS SCOREBOARD Client: Spalding Advisor: Zhao Zhang.
Final Semester 2 Presentation: April 24, Joshua Lasseigne: Team Lead and Autopilot Programming Christopher Edwards: AGL Subsystem and Website Maintenance.
Ted Hench Electronics. Our goals  Meet minimum contest guidelines with ability to expand  Stay within budget Balance the capability of our team with.
HardSSH Cryptographic Hardware Key Team May07-20: Steven Schulteis (Cpr E) Joseph Sloan (EE, Cpr E, Com S) Michael Ekstrand (Cpr E) Taylor Schreck (Cpr.
Final Presentation Senior Design II. Ralph Sandford Computer Engineer Focus: Navigation Controls Mike Smith Electrical Engineer Focus: Endurance PCB Design.
Mid Semester 2 Presentation: February 27, Joshua Lasseigne: Team Lead and Autopilot Programming Christopher Edwards: AGL Subsystem and Website Maintenance.
End of Semester 1 Presentation: November 28, 2007.
Presented by Robert Clark Instrument Technician
X-Pilot: Autopilot Solutions C. Edwards, J. Lasseigne, W. Overstreet, B. Penland X-pilot flight testing X-pilot groundstation demonstrating waypoint navigation.
Jeremy Tillman William Ehlhardt Heather Barrett Daeho Hong.
KNU RTLAB A Real-Time Linux System For Autonomous Navigation And Flight Attitude Control Of An Uninhabited Aerial Vehicle Charles E. Hall, Jr. Mechanical.
Younis H. Karim, AbidYahya School of Computer University Malaysia Perlis 1.
FlySpy Patent Liabilities Analysis
Cloud Cap Technologies
PAX River Competition UK Aerial Robotics Team University of Kentucky.
Wireless Communications Test Bed: Ad Hoc Networking
Police Car Battery Load Management
Jeff Kubascik Matt Rockey Joe Trefilek Paul Scheffler
By: Aurora Kiehl Scott Neuman Jeremie Snyder Dennis Vega Stephen Wess
Presentation transcript:

X-Pilot: Autopilot Solutions C. Edwards, J. Lasseigne, W. Overstreet, B. Penland Project Description: The X-Pilot: Autopilot Solutions project is developing a complete autopilot system (hardware in the air vehicle and groundstation software) that can be easily integrated into fixed-wing airplanes and is user programmable while in flight. The autopilot hardware is based on a Crossbow hardware platform and includes a custom- built AGL (Above-Ground-Level) sensor. The software includes the associated autopilot software along with the groundstation software. X-Pilot Components: Crossbow MNav sensor platform Crossbow Stargate Linux computer Standard wireless card Custom ultrasonic AGL sensor 6.0 Volt nickel metal hydride battery to power MNav and Stargate 9.0 Volt alkaline battery to power AGL sensor Software components for the autopilot and the groundstation (both written in C++) Hammond 1590T aluminum electrical enclosure Design Constraints and Implementation: Testing: Testing for all X-pilot components occurs in three stages. First, the component is tested with a ground software simulation. Second, the component is tested with a ground hardware simulation. Finally the component is flight tested. Current Challenges: GPS connection and functionality Converting AGL to autopilot connection from serial to USB Ground simulation tests Flight testing Areas for Improvement (second semester goals): Team X-pilot’s major second semester goal is to get the GPS unit functioning with the autopilot system. We will then shift our focus to extensive flight testing, including in-air testing of the AGL which will be on a PCB board by this time. After insuring that the system functions properly in the air and still meets all of the technical constraints, we will begin looking at adding additional features. Some of these features might include auto-takeoff, auto-landing, improved groundstation graphics and functionality, and the effect of temperature on the AGL. X-Pilot Features: Costs under $2500 Utilizes open source code for easy user modification Capable of autonomous flight by waypoint navigation Users can integrate custom hardware Equipped with an AGL for use with low level flight For use with fixed-wing or flying-wing aircraft X-pilot with labeled components Technical ConstraintDescriptionImplementation Waypoint Navigation Accuracy Waypoint navigation must be accurate to within ±10 meters. Achieved by using gains and verifying with flight log files. Low Altitude AccuracyX-pilot must be capable of accurate readings at low altitudes (±0.08 m). Low altitude accuracy achieved through an AGL using ultrasonic range finders. Real-TimeThe autopilot must have an update rate between 1 Hz and 50 Hz. By using threading, the autopilot achieved an update rate of 50 Hz. Control SurfacesX-Pilot must capable of controlled flight for a fixed-wing aircraft. X-pilot is capable of controlling the five control surfaces of a fixed-wing aircraft (two ailerons, an elevator, a rudder, and a throttle). CompatibilityThe groundstation software must be POSIX and Windows compatible. The groundstation is written in C++ and uses OpenGC. Dynamic Re-taskingX-Pilot must be capable of dynamic re-tasking at all times. The autopilot and groundstation communicate over wireless at all times so new waypoints can be uploaded at any time. Practical ConstraintDescriptionImplementation CostParts for one AGL must cost less than $200. By using ultrasonic range finders, the AGL price was kept under $200. FailsafeX-Pilot is equipped with an RC manual override. Channel 5 on the RC receiver is used to disable the autopilot mode and act as a manual override. Secure Communications Communication to the autopilot must be secure. Because an wireless router is being used, any encryption supported by the router can be implemented. Expandable DesignX-Pilot is capable of user upgrades and modifications. All software is open source, therefore the user can easily upgrade or modify the software. Operating Temperatures The system must operate in temperatures of 0- 45°C. All hardware used for X-pilot is rated for an operating temperature range of at least 0-45°C. X-pilot groundstation demonstrating waypoint navigation and one possible autopilot application—crop dusting. X-pilot flight testing Left: X-pilot autopilot software Right: Foam plane used for hardware ground testing X-pilot’s Above-Ground-Level (AGL) sensor X-pilot’s groundstation software