Deutsches SOFIA Institut Universität Stuttgart Second Gyro System for the SOFIA Telescope J.F. Wagner Deutsches SOFIA Institut, Universität Stuttgart,

Slides:



Advertisements
Similar presentations
SOFIA SOFIA Science Steering Committee Meeting Palmdale, Feb 18, 2010 Dietmar Lilienthal / Alois Himmes.
Advertisements

Leicester SRC, 3-5 Dec 2007 Systems engineering at detector level Tim Stevenson.
GLAO instrument specifications and sensitivities
The Mercury Imaging X-ray Spectrometer (MIXS): Lessons learned for the ATHENA Wide Field Imager (WFI) GW Fraser, A Martindale and C Thomas Space Research.
The New Passively Biased IFOG. A New Approach to IFOG by TeraEx Eliminating the phase modulator and its driver electronics Utilizing an innovative technique.
Return to Hubble: Servicing Mission 4 Dr. Frank Summers Space Telescope Science Institute April 2, 2009.
Optical Astronomy Imaging Chain: Telescopes & CCDs.
September, School of Aeronautics & Astronautics Engineering Performance of Integrated Electro-Optical Navigation Systems Takayuki Hoshizaki
Attitude Determination and Control
Parth Kumar ME5643: Mechatronics UAV ATTITUDE AND HEADING HOLD SYSTEM.
Attitude Determination - Using GPS. 20/ (MJ)Danish GPS Center2 Table of Contents Definition of Attitude Attitude and GPS Attitude Representations.
1 Laser Guide Star Wavefront Sensor Mini-Review 6/15/2015Richard Dekany 12/07/2009.
August, School of Aeronautics & Astronautics Engineering Optical Navigation Systems Takayuki Hoshizaki Prof. Dominick Andrisani.
Materials Science Institute 2012 Alex Muhr Jeff Shores.
ASTRI SST-2M The Prototype monolithic 1.8 m
Fiber Optic Sensors David Gunther Applied Optics 10 March 2005.
N A S A G O D D A R D S P A C E F L I G H T C E N T E R I n s t r u m e n t S y n t h e s i s a n d A n a l y s i s L a b o r a t o r y Super Star Tracker.
LIVE INTERACTIVE YOUR DESKTOP January 28, 2010 NASA/NSTA Web Seminar Series How Telescopes Have Changed Our View of the Universe Hubble’s Universe:
1 Pointing and Stabilization of Lightweight Balloon Borne Telescopes presented at the SwRI LCANS 09 Balloon Workshop on Bridging the Gap To Space Lightweight.
Computer Vision Group Prof. Daniel Cremers Autonomous Navigation for Flying Robots Lecture 3.2: Sensors Jürgen Sturm Technische Universität München.
M. Zareinejad 1. 2 Outline # Sensors –––– Sensor types Sensor examples #Actuators Actuator types Actuator examples ––––
TA Testing Plans Walter E. Miller OSC/ARC SSSC 29 September 2009.
Hubble: Back in Business and Better Than Ever Dr. Frank Summers Space Telescope Science Institute September 9, 2009.
1 SAE Aerospace Control and Guidance Systems, 2006 Lake Tahoe, NV 1-3 March 2006 Tye Brady The Inertial Stellar Compass (ISC) Tye Brady.
Accuracy Evaluation of Stereo Vision Aided Inertial Navigation for Indoor Environments D. Grießbach, D. Baumbach, A. Börner, S. Zuev German Aerospace Center.
Universität Hannover Institut für Photogrammetrie und GeoInformation Issues and Method for In-Flight and On-Orbit Calibration (only geometry) Karsten Jacobsen.
Innovative Control Systems for MEMS Inertial Sensors Michael Kraft Reuben Wilcock Bader Almutairi Fang Chen Pejwaak Salimi.
SOFIA Stratospheric Observatory for Infrared Astronomy Telescope Assembly (TA) 1 TA Activation Flight #2 “Quick Look” Data Review TA Activation Flight.
The Observations of LAMOST Jianrong Shi NAOC 1/
High Resolution Echelle Spectrograph for Chinese Weihai 1m Telescope. Leiwang, Yongtian Zhu, Zhongwen Hu Nanjing institute of Astronomical Optics Technology.
1 Stratospheric Observatory For Infrared Astronomy (SOFIA) Telescope Assembly Controlled Response Utilizing NASTRAN and MATLAB/Simulink for Pointing Analysis.
NIRSpec Operations Concept Michael Regan(STScI), Jeff Valenti (STScI) Wolfram Freduling(ECF), Harald Kuntschner(ECF), Robert Fosbury (ECF)
IMPROVE THE INNOVATION Today: High Performance Inertial Measurement Systems LI.COM.
Science - Coronal heating - Coronal structure / dynamics - Elementary processes in Magnetic Reconnection Mission instruments - Optical Telescope / Vector.
Institute of Flight Mechanics and Control Barcelona, LISA7 Symposium, June 17th 2008 IFR – University of Stuttgart LISA Pathfinder.
Effects of spatially inhomogeneous photomultiplier sensitivity….. Effects of spatially inhomogeneous photomultiplier.
1 Pointing and Stabilization of Lightweight Balloon Borne Telescopes SwRI Balloon Workshop on Low Cost Access to Near Space 27 April 2007 Larry Germann.
Chapter 20 Measurement Systems. Objectives Define and describe measurement methods for both continuous and discrete data. Use various analytical methods.
The Active Optics System S. Thomas and the AO team.
Henry Heetderks Space Sciences Laboratory, UCB
N A S A G O D D A R D S P A C E F L I G H T C E N T E R I n t e g r a t e d D e s i g n C a p a b i l i t y / I n s t r u m e n t S y n t h e s i s & A.
EE 495 Modern Navigation Systems Inertial Sensors Monday, Feb 09 EE 495 Modern Navigation Systems Slide 1 of 19.
1. 2 Content: ► 1pc Magnus Fusion Aircraft Vantage ► 1pc - Notebook based workstation for camera control and video display and storage ► 1pc - Peripherals.
Pre-focal wave front correction and field stabilization for the E-ELT
The VIRGO Suspensions Control System Alberto Gennai The VIRGO Collaboration.
M. Zareinejad 1. 2 Outline # Sensors –––– Sensor types Sensor examples #Actuators Actuator types Actuator examples ––––
EE 495 Modern Navigation Systems
Charts for TPF-C workshop SNR for Nulling Coronagraph and Post Coron WFS M. Shao 9/28/06.
Contents: 1. Introduction 2. Gyroscope specifications 3. Drift rate compensation 4. Orientation error correction 5. Results 6. Gyroscope and odometers.
MPI Semiconductor Laboratory, The XEUS Instrument Working Group, PNSensor The X-ray Evolving-Universe Spectroscopy (XEUS) mission is under study by the.
EXTP Accomodation Study Hong Bin, Zhang Long Institute of Spacecraft System Engineering. CAST Oct 27th, 2015.
PH/DT2 Scientific Tea PH-DT2 Scientific Tea, 29 April 2005 : The CMS Tracker - Mechanical Aspects Antti Onnela, PH-DT2: 1. CMS Tracker and.
EE 495 Modern Navigation Systems Inertial Sensors Wed, Feb 17 EE 495 Modern Navigation Systems Slide 1 of 18.
Strapdown Inertial Navigation Systems (INS) Sensors and UAVs Avionic
EE 495 Modern Navigation Systems
Sensor Error Characteristics By: Hector Rotstein.
Incorporating Hubble Servicing with NASA’s Long-Term Vision
SOFIA Pointing and Optimization Team (SPOT): Recent Results and Plans
FP7 LED A.Jeremie, L.Brunetti, N.Geffroy.
Fig. 1 above portrays an overall closed-loop architecture of autonomous relative navigation of a client satellite with an integrated sensor System composed.
FIZOPTIKA Sensor + Test 2017.
Intro to CCD Imaging Joe Roberts
David Gunther Applied Optics 10 March 2005
Spacecraft Attitude Determination Daniele Mortari Spring 2005
Henry Heetderks Space Sciences Laboratory, UCB
Sensors for industrial mobile Robots Incremental sensors
Validation of airborne 1
Depth Of Field (DOF).
ECE699 – 004 Sensor Device Technology
RocketSat VII Construction of an Attitude Determination System for a Sounding Rocket COSGC Symposium April 9, 2011.
Presentation transcript:

Deutsches SOFIA Institut Universität Stuttgart Second Gyro System for the SOFIA Telescope J.F. Wagner Deutsches SOFIA Institut, Universität Stuttgart, Germany

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart Wide Field Imager (WFI) Fine Field Imager (FFI) Focal Plane Imager (FPI) aircraft vibrations aero-acoustics controller commanded attitude actual attitude actuators structure and mechanics gyroscopes perturbations data fusion tracker correction Attitude Control: Inertial Stabilization + {

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart SOFIA’s Fiber Optic Gyroscopes Optical sensor module Opto-electronic module Initial situation Telescope pointing budget allocated for gyro drift: 0.04 arcsec Very low noise requirement dominated gyro design → Optical fiber length 3.4 km → Mean coil diameter150 mm → Closed loop operation Performance:Angular increment< arcsec Dynamic range> 10.3 °/s Bandwidth> 1 kHz Random walk °/√h In-run bias stability0.003 °/h

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart SOFIA’s Fiber Optic Gyroscopes

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart Constant Performance Two data sets available over a period of 9 years Data show very constant low noise behaviour Calibration 1999/2003 Calibration 2008

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart Spare part Repair Second Gyro System First possibility: Exchange of the gyro box Gyro Box 2 nd Gyro Box Nasmyth Tube ATCUTASCU Failure Gyro Box

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart Failure Second Gyro System Second possibility: Parallel system (hot standby) Gyro Box 2 nd Gyro Box Nasmyth Tube ATCUTASCU 2 nd ATCU Gyro BoxATCU

Symposium Gyro Technology Deutsches SOFIA Institut Universität Stuttgart Second Gyro System Comparison: Advantages (+) / Disadvantages (–) / Neutral (0) Gyro Box Exchange Hot Standby Accuracy+– Cost–– Software modification0– ATCU failure– ++ “Save a mission”–++ Flexibility of schedule– +