1 / 8

Minnesat University of Minnesota Jason Mintz Jim Pogemiller Abdul Azeem Khan Vincent Jusuf

Minnesat University of Minnesota Jason Mintz Jim Pogemiller Abdul Azeem Khan Vincent Jusuf. SHOT II Presentation. Mission Overview. Collect GPS sensor data in an atypical environment Compute payload attitude from GPS sensor data Compare GPS attitude to attitude from MIDG INS.

gezana
Télécharger la présentation

Minnesat University of Minnesota Jason Mintz Jim Pogemiller Abdul Azeem Khan Vincent Jusuf

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. MinnesatUniversity of Minnesota Jason Mintz Jim Pogemiller Abdul Azeem Khan Vincent Jusuf SHOT II Presentation

  2. Mission Overview • Collect GPS sensor data in an atypical environment • Compute payload attitude from GPS sensor data • Compare GPS attitude to attitude from MIDG INS

  3. SHOT II / UN-4 Connection • Minnesat Mission Statement: The purpose of Minnesat is to design, construct, and validate an ultra-short baseline GPS attitude determination system in Earth orbit. • SHOT II experiment will verify ultra-short baseline design approach of GPS attitude determination system • SHOT II experiment will test algorithms used to compute attitude from GPS receivers

  4. SHOT II Design and Test Details • SHOT II payload structural design: • Aluminum GPS housing • Foam-core housing • Polyethylene wrap insulation • Composite antenna mounting arm • SHOT II payload electrical design: • 4 A hr, 2 cell (7.4 V) Li-Poly battery • Step down DC regulator to power GPS receivers & Computers (7.4 V  5 V) • 9 Volt Battery to power MIDG unit

  5. SHOT II Design and Test Details • SHOT II experiment design: • 4 GPS antennas  4 GPS receivers ( 1 per antenna) • Antennas mounted to replicate baselines between GPS antennas on Minnesat • MIDG IMU truth system • 5 GUMSTIX Computers • Data logger: one for each receiver & MIDG • Test program: 2 hour functional test • Verify operation in extreme temperature cases: • Hot case on hot rooftop • Cold case in dry ice cooler • User Guide Compliance • Mass • Payload Interface: Polyethylene tubing, Washers & Pins (Similar to SHOT I) • Electrical grounding: GPS box • Battery powered: Li-Poly  GPS, GUMSTIX & 9 Volt  MIDG

  6. Expected results

  7. Expected Results

  8. Demonstration

More Related