RIT Space Exploration Group (SPEX)

Slides:



Advertisements
Similar presentations
Design and Simulation of the Attitude Determination and Control System for LightSail-1 Matt Nehrenz.
Advertisements

Bryan Sonneveldt Mentor: Dr. Iman Alizadeh School of Earth and Space Exploration and Ira A. Fulton Schools of Engineering at Arizona State University Small.
TCS3 Servo System Proposed Design. Why Model? Meet Resolution Requirements What Resolution Encoder to use? Velocity Configuration PID Values Wind Loading.
Attitude Determination and Control System Peer Review December 2003.
Kedrick Black1 ECE 5320 Mechatronics Assignment #1 Torque Coils/Rods and Reaction Wheels Kedrick Black.
Attitude Determination and Control
Unit 4 Day 3 – Magnetic Dipole Moment & Applications
Karla Vega University of California, Berkeley Attitude Determination and Control 6/9/2015.
Satellite Overview Size does count. “Design is an iterative process. The necessary number of iterations is one more than the number you have currently.
1 Handout #17 Tennis racket demo Euler’s equations Motion of a free body No external torques Response to small disturbances  Tennis racket theorem  Nutation.
Earth Science Projects for Olin College Students: J. Vanderlei Martins UMBC Physics Department and NASA GSFC Climate and Radiation Branch 1. CCD Detection.
Magnetism (sec. 27.1) Magnetic field (sec. 27.2) Magnetic field lines and magnetic flux (sec. 27.3) Motion of charges in a B field (sec. 27.4) Applications.
Magnetism (sec. 27.1) Magnetic field (sec. 27.2) Magnetic field lines and magnetic flux (sec. 27.3) Motion of charges in a B field (sec. 27.4) Applications.
Feasibility of Demonstrating PPT’s on FalconSAT-3 C1C Andrea Johnson United States Air Force Academy.
November 21, 2014 Mars Cubesat/Nanosat Workshop Flux-Pinned Interfaces for Martian Applications Laura Jones G&C Systems Engineer, Jet Propulsion Laboratory,
Choose the right picture
Gyroscopic attitude control systems
DC motor model ETEC6419. Motors of Models There are many different models of DC motors that use differential equations. During this set of slides we will.
Attitude Determination and Control System
Attitude Determination and Control System (ADCS)
Active magnetic attitude control system providing three-axis inertial attitude M. Ovchinnikov, V. Penkov, D. Roldugin, A. Guerman Keldysh Institute of.
RoboTeam 9/1/2011 Preformed by:Costia Parfeniev, Boris Pinzur Supervised by: Kobi Kohai.
Disturbance Rejection: Final Presentation Group 2: Nick Fronzo Phil Gaudet Sean Senical Justin Turnier.
Thursday, Nov. 3, 2011PHYS , Fall 2011 Dr. Jaehoon Yu 1 PHYS 1444 – Section 003 Lecture #18 Thursday, Nov. 3, 2011 Dr. Jaehoon Yu Torque on a Current.
Week 7 Status Updates. Statement of Work: To design and prototype an attitude control system (ACS) for a Cube-Sat. This ACS will align the Cube-Sat with.
II Explanation of the Electric Motor Demonstrated in Class.
 Define engine  Define motor  Describe the difference between the two.  Describe how both operate.
1 Weekly Summary Weekly Summary Formation Flight AEM4332 Spring Semester March 7,2007 Masao SHIMADA.
Capstone Design Team. CHI-A 정준영 전우준 김건식 김병찬 한일환
General Physics 2Magnetism1 Mass Spectrometer Used to identify atoms and their concentrations in a sample of material. Between S1 and S2, molecules go.
CubeSat for Ions, Neutrals, Electrons and Magnetic Fields PI Robert Lin, SSL Project Manager Thomas Immel, SSL System Engineer David Curtis, SSL STEIN.
Introduction: The on-board measurements available for control are a dual-slit sensor to find the elevation of the sun and a magnetometer to measure the.
GLAST Science Support Center July 16, July Ground Software Workshop The Spacecraft Simulator David S. Davis, GSSC.
Hi6Hi5 Hi2 Hi4 Hi3 Product (assembly) xz – horizontal plane.
Advanced Application of Flywheels Cory Markham. Components of a flywheel energy storage system  Rotor: spinning mass that stores energy  Bearings: pivots.
Electrodynamic Tether Payload RIT SPEX Acknowledgements This work was supported by Provost’s Learning Innovation Grant, Kate Gleason College.
1 Weekly Summary Solar Sail Spring Semester March 19 th, 2007 Mike Hiti.
TRIO-CINEMA 1 UCB, 2/08/2010 ACS Dave Auslander, Dave Pankow, Han Chen, Yao-Ting Mao, UC Berkeley Space Sciences Laboratory University of California, Berkeley.
Robotics Grant Agreement No LLP UK-LEONARDO-LMP Project acronym: CLEM Project title: Cloud services for E-Learning in Mechatronics Technology.
KUFASAT STUDENTS’ SATELLITE
Environment Simulator
Smart Nanosatellite Attitude Propagator ssl.engineering.uky.edu/snap
Electricity and Magnetism
Aerodynamic Attitude Control for CubeSats
AUTOPILOT The autopilot or automatic pilot is a system of automatic controls that holds the aircraft on any selected magnetic heading & returns the aircraft.
Star Detection and Tracking Embedded Linux Hardware
Module roadmap to end of 2017
Voice of the Customer Presentation
Ch 7 Objective Warm-Up You will learn about circular acceleration and Force You will learn to use Newton’s Universal Gravitation formula You will learn.
Fault Operations Software Team System-Level Software Health
ACS UC Berkeley Space Sciences Laboratory
Satellite Attitude Dynamics & Control System (ACS) Testbed
PHYSICS 197 Section 1 Chapter C7 Angular Momentum
Virginia CubeSat Constellation
ERV Design Chris Heidelberger Dynamics & Control
Matthew Prevallet 4/26/16 Arizona/NASA Space Grant Symposium
Kletskous Magnetic Stabilization
Earth Demo The movements of the Earth cause day and night, as well as the seasons. We will explore Earth’s movements. Model rotation. Model revolution.
Performance Test of a Fluidic Momentum Controller in Three Axes
אביבה אלקלעי, ראש היחידה לכניסה להוראה, המכללה האקדמית אחווה
מהו הסטאז'? המכללה האקדמית תלפיות.
Design & Development of a Quad Rotor MAV Beniamin Apopei
Attitude Determination and Control Preliminary Design Review
Mark Suder
Attitude Determination Overview
Sub-Orbital CubeSat Experimental Mission
Innovative Motor Designs for Electric Cars Come to Life
Team P16228: Magnetically Levitated Propeller
Prof. Leonardo M. Reyneri
Laboratory for Advanced Space Systems at Illinois
Presentation transcript:

RIT Space Exploration Group (SPEX) ADCS Attitude Determination and Control System

Control Moment Gyro Create a single DOF Control Moment gyroscope https://www.youtube.com/watch?v=5cRb0xvPJ2M Test bed for control system development Validate Matlab Simulations Develop CMG control system Use MSP430 Position control Disturbance rejection Motor Desaturation Current State Most components machined Ordering final components

Magnetorquer Demo Create a Magnetorquer Demo for Imagine RIT Demonstrate attitude control using earth’s magnetic field Create test bed for attitude control systems Create first generation system that can be improved for 1U CubeSat Work to be done: Finish choosing components Order parts for system Assemble magnetorquers & supporting circuitry

GMAT/STK Simulation Understand Capabilities of Orbital Software Learn how to incorporate orbital information into attitude simulations Begin building attitude simulations Simulate CubeSat rotation in orbit Account for disturbance torques Account for Magnetorquer torques

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

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