Scott A. Kowalchuk Advisor: Dr. Christopher Hall

Slides:



Advertisements
Similar presentations
Solar Sail Attitude Control using a Combination of a Feedforward and a Feedback Controller D. Romagnoli, T. Oehlschlägel.
Advertisements

Design and Simulation of the Attitude Determination and Control System for LightSail-1 Matt Nehrenz.
Nonlinear dynamics of a rotor contacting an elastically suspended stator 1 st International Conference on Vibro-Impact Systems Loughborough, UK, July 20-22,
Honor Thesis Presentation Mike Bantegui, Hofstra University Advisor: Dr. Xiang Fu, Hofstra University EFFICIENT SOLUTION OF THE N-BODY PROBLEM.
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,
Scaled Helicopter Mathematical Model and Hovering Controller Brajtman Michal & Sharabani Yaki Supervisor : Dr. Rotstein Hector.
Optical Navigation System Michael Paluszek, Joseph Mueller, Dr. Gary Pajer Princeton Satellite Systems EUCASS July 4-8, 2011 St. Petersburg, Russia.
Middle East Technical University Aerospace Engineering Department STEERING LAWS FOR CONTROL MOMENT GYROSCOPE SYSTEMS USED IN SPACECRAFTS ATTITUDE CONTROL.
CSE115: Introduction to Computer Science I Dr. Carl Alphonce 219 Bell Hall
A De-coupled Sliding Mode Controller and Observer for Satellite Attitude Control Ronald Fenton.
A Survey of Some Sliding Mode Control Designs Dennis Driggers EE691 March 16, 2006.
Jesus Benhumea Kevin Stokely Matt Aggleton Advisor: Dr. Scott Franklin Jamming in 2-D Prolate Granular Material Systems. *Petroleum Research Fund #39132-GB9.
11/28/06Preliminary Design1 Automated Excel Grading System Welcome Ms. Jami Cotler and Dr. Scott Hunter And Guests.
AAE 666 Final Presentation Spacecraft Attitude Control Justin Smith Chieh-Min Ooi April 30, 2005.
System for Engine Location Of a Web Train Paul Wimmer and Adam Weintrop Dr. Irwin and Dr. Schertz 12/5/05 Project Proposal -CTCDS.
February 24, Final Presentation AAE Final Presentation Backstepping Based Flight Control Asif Hossain.
Intro to Satellite Orbits Introduction to Space Systems and Spacecraft Design Space Systems Design.
Linearisation about point equilibrium n-dimensional autonomous a constant / point equilibrium solution of the dynamics a ‘neighbouring’ solution first-order.
Introduction to Space Systems and Spacecraft Design Space Systems Design Satellite Operations.
Performance Guarantees for Hazard Based Lateral Vehicle Control
System for Engine Location of the WebTrain Adam Weintrop and Paul Wimmer Advisors Dr. Irwin and Dr. Schertz.
Physics 218: Mechanics Instructor: Dr. Tatiana Erukhimova Lecture 21 Hw: Chapter 13 problems and exercises.
1 Test Slide Text works. Text works. Graphics work. Graphics work.
FPGA based RFID Reader Group Members – Farhan Tariq Usman Sarwar Khalid Khan Supervisor- Mr. Naveed Ahmed Internal Advisor- Prof. Dr. Abdul Razzak Memon.
Closed Loop Magnetic Levitation Control of a Rotary Inductrack System Students: Austin Collins Corey West Advisors: Mr. S. Gutschlag Dr. Y. Lu Dr. W. Anakwa.
Integrated Orbit and Attitude Control for a Nanosatellite with Power Constraints Bo Naasz Matthew Berry Hye-Young Kim Chris Hall 13th Annual AAS/AIAA Space.
EE/CS 480 Fall /8/2015 9:05:03 AM University of Portland School of Engineering Project STEEL Bridge Program Review 1 Team Shawn Patterson Chris.
EE/CS 480 Fall /8/2015 9:09:41 AM University of Portland School of Engineering Project STEEL Bridge Program Review 2 Team Shawn Patterson Chris.
Reconfigurable Communication System Design
ICRA ’07 Space Robotics Workshop A Form Based Control Algorithm for Reducing the Complexity of an Attitude Control System at ICRA 2007 Space Robotics Workshop.
1 Adaptive, Optimal and Reconfigurable Nonlinear Control Design for Futuristic Flight Vehicles Radhakant Padhi Assistant Professor Dept. of Aerospace Engineering.
Geometric Spin Hall Effect of Light Andrea Aiello, Norbert Lindlein, Christoph Marquardt, Gerd Leuchs MPL Olomouc, June 24, 2009.
Guidance, Navigation and Controls Subsystem Winter 1999 Semester Review.
1. Warm-Up 3/31 C. Rigor: You will learn how to solve polynomial inequalities and rational inequalities. Relevance: You will be able to use polynomial.
Aeronautics & Astronautics Autonomous Flight Systems Laboratory All slides and material copyright of University of Washington Autonomous Flight Systems.
ABL Tracking System PRESENTED BY: SIDNEY JONES AND AJ MARIN.
Using Kalman Filter to Track Particles Saša Fratina advisor: Samo Korpar
Adaptive Optimal Control of Nonlinear Parametric Strict Feedback Systems with application to Helicopter Attitude Control OBJECTIVES  Optimal adaptive.
SSE-120 Understanding Orbits Questions 1. Why are the suns rays shown as parallel when reaching the earth? 2. Does the earth have the axis tilted all year.
Penn State, 20 th -24 th July TH INTERNATIONAL LISA S YMPOSIUM D. Bortoluzzi, M. Da Lio, S. Vitale1 LTP dynamics and control D. Bortoluzzi, M. Da.
11-1 Lyapunov Based Redesign Motivation But the real system is is unknown but not necessarily small. We assume it has a known bound. Consider.
Terrain Reconstruction Method Based on Weighted Robust Linear Estimation Theory for Small Body Exploration Zhengshi Yu, Pingyuan Cui, and Shengying Zhu.
Ping-Pong Ball Levitation
Date of download: 10/29/2017 Copyright © ASME. All rights reserved.
S.A.I.L.S. Sailing using An Intelligent Logistician System
Rajagopal, Harish Nawani, Varun
What type of spacecraft is this? What might be its purpose?
  Figure 7.1 Track Layout with Input Sensors and Output Switches and Output Tracks.
Consider the effective potential
Team Members Class and Date
Sun – Earth System Questions
E190Q – Final Project Presenation
Instructor: Dr. Tatiana Erukhimova
Recent works of Attitude Control System for GAPS
Project Sublimity Audio Stereo Class-D Audio Amplifier
  Figure 8.1 Track Layout with Input Sensors and Output Switches and Output Tracks.
Research project summary Objectives for the current period
Multiscale Modeling of Flood-Induced Surface Erosion in a Particle Bed
Session 6 Aeronomy/ Novel applications
Rice University Darren Homrighausen David Kahle July 29th, 2005
Team Dustin Digmann Philip Johnston Tobias Scherf
What type of spacecraft is this? What might be its purpose?
Development of a new approach for modelling wave energy converters
12cm Area 64cm2 Area 100cm2 ? ? Area ?cm2 12cm Area 36cm2
Dynamic Modeling PDR Dynamic Modeling Preliminary Design Review for Vehicle and Avionics October 17, 2000 Presented By: Christopher Peters …and that’s.
Graduation Project Project Name
Scaling Behavior in the Stochastic 1D Map
12cm Area 64cm2 Area 100cm2 ? ? Area ?cm2 12cm Area 36cm2
Polynomial Functions and Models
Current Status of Ion Polarization Studies
Presentation transcript:

Scott A. Kowalchuk Advisor: Dr. Christopher Hall ATTITUDE CONTROL INVESTIGATION USING SPACECRAFT HARDWARE-IN-THE-LOOP SIMULATOR Scott A. Kowalchuk Advisor: Dr. Christopher Hall

Overview Hardware-in-the-loop Attitude Spacecraft Simulator Nonlinear Attitude Controller Attitude Control Simulation Results Control Simulation Video Conclusions

Simulator Diagram

Nonlinear Attitude Controller EOM: Candidate Lyapunov Function: Control: Simulator Control:

MRP Controller Results

MRP Controller Results

Control Simulation Video

Conclusions Attitude and angular rates go to zero Results match numerical simulation Future Plans Tracking Problem Coupled Attitude and Orbit Control using GPS hardware-in-the-loop Simulator

Feedback: Privacy Policy Feedback
Do Not Sell My Personal Information
About project: SlidePlayer Terms of Service

© 2025 SlidePlayer.com. Inc. All rights reserved.