Marc Walch Page 1 CNES’07 Peer Review 4/17/02 Wide Angle Camera (WAC) And Narrow Angle Camera (NAC) Marc Walch April 17, 2002 CNES’07 Mars Premier Peer.

Slides:

Advertisements

Similar presentations

EIS/Solar-B: 3. Electrical Interface to MDP EISMDP PIM HK PIM DHU DR analog data (temperature, current, etc.) S/C bus image compression status data command.

Advertisements

Octavian CRISTEA1, Paul DOLEA1, Vlad TURCU2, Radu DANESCU3

Available in Black and Silver The all-in-one camera.

1 FGS Guider CDR – April 19, 2007 © Copyright 2007 Her Majesty the Queen in Right of Canada Subject to Controlled Goods Regulations of Canada FGS Guider.

Instrument Checkout / Performance Verification for XRT & Control of XRT Observation R. Kano for the XRT Team.

Using DELPHI for Weak Lensing Measurements: Science Return and Mirror Size Jes Ford, JPL, UNR SURF /21/07 Mentor: Jason Rhodes Co-mentor: David Johnston.

LXO/MagEX Meeting Greenbelt, 24/10/07 Telescope Baseline Configuration: Imaging Capability (Micropore Optic) Telescope Field of View ~ 30° x 30° Angular.

School of Earth and Space Exploration Existing Lunar Datasets M. S. Robinson School of Earth and Space Exploration Arizona State University.

SDW20051 Vincent Lapeyrère LESIA – Observatoire de Paris Calibration of flight model CCDs for CoRoT mission.

Aloha Proof Module Design Cabled Observatory Presentation School of Ocean and Earth Science and Technology February 2006.

Tight environment high radiation area non-serviceable area passive components optics only, no active electronics transmit image through flexible fiber.

PLATO kick-off meeting 09-Nov-2010 PLATO Payload overall architecture.

Cube Root Georgia Institute of Technology Matt Bigelow, Gregory Hansen, Sarah McNeese, Luke Walker.

On A Large Array Of Midsized Telescopes Stephen Fegan Vladimir Vassiliev UCLA.

Detection of Terrestrial Extra-Solar Planets via Gravitational Microlensing David Bennett University of Notre Dame.

Author Name Page 1 CNES’07 Peer Review 4/17/02 CNES’07 Mars Premier Peer Review Rendezvous and Sample Capture OS Beacon Electronics And Power System Mark.

Proposed US Contribution to the Wide Field Imager PSU MIT JHU.

Eddington Kick-Off. Vienna, September 17th, 2001 T.Muñoz/C.Laviada (INTA) 1 EddiCam: The Eddington Photometric Camera Preliminary Design Layout.

1 Mirror subsystem: telescope structure Functions: Functions: Support mirrors subsystem to S/C Support mirrors subsystem to S/C Accommodate cryostat Accommodate.

ISUAL Test Verification Matrix H. Heetderks. TRR December, 20002NCKU UCB Tohoku ISUAL Verification Matrix Heetderks Verification Matrix -- Imager Related.

ISUAL Sprite Imager Electronic Design Stewart Harris.

7/12/20011 Observing Sequences in View of the SECCHI Science Goals From the EUVI Perspective J-P. Wülser.

Brief introduction of YINGHUO-1 Micro-satellite for Mars environment exploration J. Wu, G. Zhu, H. Zhao, C. Wang, L. Lei, Y. Sun, W. Guo and S. Huang Center.

Life in the Atacama, Design Review, December 19, 2003 Carnegie Mellon SPI and Context Imagers Life in the Atacama Design Review December 19, 2003 Stuart.

Institute: ISE, group: PERG CCD USB 2.0 Camera for the Pi of The Sky Project Grzegorz Kasprowicz semester: T1EL-PE Cooperation with Soltan Institute for.

JPL AUTONOMOUS RENDEZVOUS OVERVIEW Rob Bailey Jet Propulsion Laboratory Inter-Agency AR&C Working Group Meeting May , 2002 Naval Research Laboratory.

Lecture Exposure/histograms. Exposure - Four Factors A camera is just a box with a hole in it. The correct exposure is determined by four factors: 1.

Leo Greiner TC_Int1 Sensor and Readout Status of the PIXEL Detector.

Solar-B SOT/FPP 1 SOT April 2006Ted Tarbell FPP CCD Camera Performance Ted Tarbell 17-Apr-2006.

XRT’s Observational Parameters R. Kano (NAOJ). Contents FOV & Full Disk Imaging Time Cadence & Observation Table New Items as Solar X-ray Telescopes –Pre-flare.

Standard Form Recap – Planetary Data Sun mass kg.

Features of the new Alibava firmware: 1. Universal for laboratory use (readout of stand-alone detector via USB interface) and for the telescope readout.

The Taiwanese-American Occultation Survey (TAOS) Matthew Lehner ASIAA.

1 NAC-Slide: Displaying Very Large NAC Images Robert Wagner Mentor: Mark Robinson School of Earth and Space Exploration, ASU 17 April 2010.

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.

Cellular-Enabled Remote Camera System. Team Members Damion Cuevas Power Systems Sensors Research Josh Lunn Hardware interfacing Web page design Research.

Cellular-Enabled Remote Camera System. Team Members Damion Cuevas Power Systems Sensors Research Josh Lunn Hardware interfacing Web page design Research.

Final Slides By: Kara Akgulian Mission Ops Locomotion Phase 1.

Telescopes Resolution - Degree to which fine detail can be distinguished Resolution - Degree to which fine detail can be distinguished Fundamentally an.

No Blur in the Image Sensor Consistent light. Motion Blur in the Image Sensor Inconsistent light.

Navigation and Ancillary Information Facility NIF SPICE Geometry Finder (GF) Subsystem Searching for times when specified geometric events occur September.

STAR Pixel Detector readout prototyping status. LBNL-IPHC-06/ LG22 Talk Outline Quick review of requirements and system design Status at last meeting.

Cellular-Enabled Remote Camera System. Team Members Damion Cuevas Power Systems Sensors Research Josh Lunn Hardware interfacing Web page design Research.

ISUAL System Design H. Heetderks. PDR 31 August 2000NCKU UCB Tohoku ISUAL System Design H. Heetderks 2 ISUAL Operations Overview.

Pre-decisional – for Planning and Discussion Purposes Only 1 Technology Planning for Future Mars Missions Samad Hayati Manager, Mars Technology Program.

Night Sky Video Observation Equipments  Video cameraVideo camera  LensLens  A/D converterA/D converter  PC for UFOCapturePC for UFOCapture  Housing/MountHousing/Mount.

for Lomonosov-GRB collaboration

H. U. Keller, M. Küppers, L. Jorda, P. Gutierrez, S. Hviid, C

Ball Aerospace Scalable Configurable Cryocooler Electronics (SCCE)

Rosetta’s first view of CG

E. Ponce2-1, G. Garipov2, B. Khrenov2, P. Klimov2, H. Salazar1

ISUAL Imager Stewart Harris.

OSIRIS Full Team Meeting Welcome, Introduction, Logistics

Lessons learnt from the STEREO Heliospheric. Imagers: Tracking

Summary of the science planned per mission phase

OSIRIS operation summary

Mini-RF Requirements Overview

The Lunar Reconnaissance Orbiter

Lunar Reconnaissance Orbiter Camera

Rover Communication Subsystems

Image Frame As camera shakes/rotates, the image frame that it covers (“field of view”) shifts Capturing inconsistent image yields blur.

Image Frame As camera shakes/rotates, the image frame that it covers (“field of view”) shifts Capturing inconsistent image yields blur.

Standard Form Recap –.

درس تكنولوژي‌هاي ارتباطي دانشگاه علامه طباطبايي

Observational Prospect of NIREBL

Worldview II Launched October 8, 2009 Altitude: 770 km

Standard Form Recap –.

ABB-Welcome Video Indoor Station 7”

ME instrument and in-orbit performance

CHEOPS - CHaracterizing ExOPlanet Satellite

Presentation transcript:

Marc Walch Page 1 CNES’07 Peer Review 4/17/02 Wide Angle Camera (WAC) And Narrow Angle Camera (NAC) Marc Walch April 17, 2002 CNES’07 Mars Premier Peer Review Rendezvous and Sample Capture

Marc Walch Page 2 CNES’07 Peer Review 4/17/02  NAC  Build to print MRO OptNav Camera, use of spare MRO parts  Detect OS at 3,000 km  Relative motion requirement (OS in FOV) TBD  Resolve OS down to 10 m (may be too bright?)  Image update rate 20 seconds or less (data in S/C buffers within 20 seconds from end of exposure)  Variable/commandable exposure times  WAC  Build to print or spare MER NAV Camera  Detect OS at 2 km  Relative motion requirement (OS in FOV) TBD  Resolve OS to 2 m  FOV at least 40 degrees (full cone angle - covers expected proximity ops OS to camera relative motion)  Image update rate 5 seconds or less (data in S/C buffers within 5 seconds from end of exposure)  Variable/commandable exposure times Requirements

Marc Walch Page 3 CNES’07 Peer Review 4/17/02  Both  Ariane V launch environment.  Grade 2+ parts.  Other  Mission Assurance Class B+ mission Grade 2+ parts 18 kRad total dose  OS 20 cm diameter, 0.5 albedo, 30% return for Sun angle 3000 km range for search mode 2 km range for terminal phase mode Requirements

Marc Walch Page 4 CNES’07 Peer Review 4/17/02  Mechanical Drawing NAC Specifications

Marc Walch Page 5 CNES’07 Peer Review 4/17/02 NAC Specifications Power Supply (red box) Regulators, S/C interface, FPGA, ADC (green box) Radiator

Marc Walch Page 6 CNES’07 Peer Review 4/17/02  Performance  Power2.5 W  Mass2.5 kg (includes radiator and mount)  FOV1.4º  InterfaceLVDS (Command & Data, each having 3 lines)  Data transfer rate1 MHz baseline, 3 full-frame buffer  Resolution1 pixel = 20 cm at 8,500 m NAC Specifications

Marc Walch Page 7 CNES’07 Peer Review 4/17/02 WAC Specifications  Mechanical Drawing

Marc Walch Page 8 CNES’07 Peer Review 4/17/02  Performance  Power2 W continuous, some peaks at 3 W (readout & flush)  Mass235 g  FOV45º  Best focus1 m  Depth/field0.5 m  infinity  InterfaceLVDS (Command –2 lines– and Data – 3 lines –)  Data transfer rate10 MHz baseline (1 full frame in ~5 s)  In-spec T-55 C  +22 C  Survival T-120 C  +70 C WAC Specifications