SNUSAT-1 for QB50 Project SNUSAT-1 Orbit Specification Altitude: 320km Inclination: 79 degrees Orbit Period: 90.85 minutes Orbit life: 90 days Attitude.

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Presentation transcript:

SNUSAT-1 for QB50 Project SNUSAT-1 Orbit Specification Altitude: 320km Inclination: 79 degrees Orbit Period: minutes Orbit life: 90 days Attitude Control Specification Reaction Wheel & magnetorquer to obtain 5 degrees stability Development of Electrical Systems - Electrical Interface - Harness Design - Development of Magnetic torquer Secondary: FDIR algorithm validation Drag coefficient modeling Imaging of COTS CMOS Primary: Lower thermosphere exploration (FIPEX Sensor Used) Missions Communication Specification Downlink: 433MHz Uplink: 145MHz

ARLISS Cansat Competition Autonomous Control of Rover using GPS Robust design for rocket launch and safe descent Communication between Satellite and Rober Pickup Mechanism for Satellite Pickup Responsible for Satellite Hardware

Vision Guidance Filming Drone Excellence Prize, Creative Design Fair, Seoul National Univseristy, Oct.2013 Bronze Prize, International Capstone Design Fair, Korea Univsersity, Nov.2013 Bronze Prize, Electronics Fair, Seoul National University, Nov.2013 Following protagonist using vision guidance Flight data visualization for confirmation of the operator Detection of Marker Position/ Orientation Jaeyoung Lim, Jaemin Cho, Sanghyun Hong, Dongho Kang

Teleoperated Drone Experiment - First-Person-View operation using head mounted display and head trackers - Flight data displayed on-screen using OSD - Follow me mode using Droid Planner on a mobile device

Quadcopter for 350ml Class Cansat Deployment Heavylift Multirotor for Cansat Deployment - Max Payload: 4kg (15Minutes Flight Time) - GPS enabled position control - Max Payload: 500g -GPS enabled position control -350ml Cansat deployer developed - Undergraduate Research Program - student research seminar ( 자율연구 )