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8 Roll Field of Regard Pitch Field of Regard On-orbit adjustability Margin Margin 5 10 Margin Nominal Margin Margin Station-Keeping 9.4 m (Membrane) +V 9.8 m (Membrane) 12.7 m 2.3 m 4.3 m +J

10 ISIM

11 NIRCam Fine Guidance Sensor MIRI NIRSpec

12 Fixed Solar Arrays (1 of 2) High-gain Gain Antenna (Ka Band and S Band) 1-lb 1lb Dual-thruster Thruster Modules (1 (1 of of 4) Stationkeeping Thruster Deployable Radiator Shad Star Trackers (3) Radiator Surface Coarse Sun Sensors (2 of 4) Fine Sun Sensor 5-lb Dual Thruster Modules (1 of 2)

Integrated Science Instrument Module ISIM Thermal Enclosure Aft

13 Telescope Structure Primary Mirror: 18 hexagonal segments, 1.3 m flat to flat, <25 nm rms surface Secondary Mirror Integrated Science Instrument Module ISIM Thermal Enclosure Aft Optics Subsystem: Tertiary Mirror Fine steering Mirror Sunshield Spacecraft

ITT JWST prime contractor Optical system development Telescope integration and test Telescope structure Observatory performance and programmatics Systems

Element (OTE) optical design and optics Beryllium mirror segment development and cryogenic testing Wavefront Sensing & Control (WFS&C) design and algorithms

14 ITT JWST prime contractor Optical system development Telescope integration and test Telescope structure Observatory performance and programmatics Systems engineering and interfaces Spacecraft, sunshield, and deployables Observatory integration and test Support ground segment and operations Optical Telescope Element (OTE) optical design and optics Beryllium mirror segment development and cryogenic testing Wavefront Sensing & Control (WFS&C) design and algorithms OTE and observatory AI&T support OTE ground AI&T Plum Brook test configuration and interfaces Telescope backplane and Secondary Mirror (SM) support structure design and build

15 ESA/European Consortium NIRSpec Instrument MIRI optical bench assembly and instrument integration and test Ariane 5 launch vehicle CSA FGS with tunable filter modules University of Arizona NIRCam instrument (subcontracted to Lockheed-Martin ATC) JPL MIRI management and systems engineering team lead, flight software focal plane array/focal plane electronics (FPA/FPE) and dewar WFS&C technology development and oversight MSFC Mirror technology development and testing Environmental analysis AMES Detector technology development

24 PERIHELION (4Rs) October 2010 EARTH at PERIHELION o (at Quadrature: Sun - S/C - Earth angle = 90.0 ) o POLAR ORBIT (i = 90.0 ) 50 d JUPITER GRAVITY ASSIST FLYBY June 2007 LAUNCH February C 3 = 110 km /sec (Delta III/Star 48 ~ 300 kg)

25 Rs o o o o o Rs Delivery Error ΔB*R=450 km (3σ) ΔB*T=46.8 km (3σ) o l = 90 o R-Axis (km*10 ) Rx Rp=4.0 Rs o o Rs o Rs o Rs ΔR s = Δi = 0.03 Rs 0.02 o o Rs T-Axis (km*10 ) 215 Rs 165 Rs (1.0 AU) (0.8 AU) -30 d -25 d -20 d Start Encounter -15 d Plasma Observations +30 d ECLIPTIC PLANE +25 d +20 d +15 d 104 Rs (0.5 AU) -10 d +10 d Far Encounter Configuration with Aft Boom Extended 65 Rs (0.3 AU) -5 d -1 d 20 Rs -1 d +5 d +1 d End Critical Science Acquisition Begin Critical Science Acquisition -22 hrs -18 hrs Nadir Pointed Spacecraft (typ.) High Speed Solar Wind Zone -14 hrs -10 hrs -8 hrs -6 hrs -4 hrs -2 hrs 0 hrs +2 hrs +4 hrs +6 hrs +8 hrs +10 hrs +14 hrs +18 hrs +22 hrs High Speed Solar Wind Zone Low Speed S/W Zone

26 Primary Shield / Antenna Primary Shield Support Struts EUV Imager Y X Optical Collimators Secondary Heat Shields (2) Nadir Viewing Plasma Spectrometer Coronagraph (2) Avionics Panel (4) Stellar Reference Units (2) Spacecraft Bus Umbra at Perihelion Low Gain Antenna (2) Thruster Cluster (4) Radioisotope Power Source Telescopic Science Boom (in retracted position) Aft Plasma Spectrometer and Triaxial Magnetometer Z Tungsten Feed Element Coaxial Tube (CMC) 35 cm X - Band Waveguide (CMC)

35 UE+ Terrestrial repeater Unicast return channel over GPRS RNC SDMB Hub T-UMTS Network SGSN GGSN SSN Gi* MBMS Broadcast Mode over SDMB Gmb* Gi BM-SC Gmb Content providers or multicast sources MBMS Multicast Mode over T - UMTS

To S-HUB Fully trust Gi* Gi Gi/Gmb Gi*/Gmb* Gi* BM -SC Gmb Security function Membership function Gi*/Gmb Proxy and

36 Bearer management processes Higher layers (peered with UE) DIAMETER / RADIUS TCP / UDP DIAMETER / RADIUS TCP / UDP IP PDCP IP L2 Phy IP L2 Phy IP / IP-Sec L2 IP / IP-Sec L2 SDMB Network Hub Gi* BM-SC Phy Phy Hub Gmb* BM-SC To UE To GGSN To S-HUB Fully trust Gi* Gi Gi/Gmb Gi*/Gmb* Gi* BM -SC Gmb Security function Membership function Gi*/Gmb Proxy and Transport function Path choosing function Session and Transmission function Content Provider Service announcement function

37 Control-plane RRC User-plane Radio Resource Assignment User-plane [Code, Frequency, TS, TF Set, Mapping, etc.] Control-plane RRC Control PDCP PDCP Control Measurements Control R L C R L C Control Measurements M A C UE from SDMB PHY Uu* M A C SDMB HUB to SDMB PHY

38 Logical Channels DTCH DCCH MTCH MCCH MSCH BCCH MCCH MSCH PCCH MAC Transport Channels DCH DSCH FACH PCH BCH PHY Physical Channels DPDCH DPCCH PDSCH S-CCPCH P-CCPCH CPICH AICH AP-AICH SCH MICH CSICH CD/CA-ICH

39 UE IMR SAT RNC SDMB Hub SSN BM-SC 1. Session Start Request 1. Session Start Response 2. MBMS Session Start Request 2. MBMS Session Start Response 3. Radio Bearer Establishment in SDMB RNC 4. MBMS Notification on MICH 5. MBMS Radio Bearer Information on MCCH/FACH 6. Radio Bearer Establishment in UE 7. MBMS Scheduling Information on MSCH/FACH 7. MBMS data on MTCH/FACH 7. MBMS data 7. MBMS data

40 Logical channel Transport channel Physical channel Logical channel Transport channel Physical channel MTCH 1 MTCH 2 MTCH 3 MTCH 4 FACH 1 FACH 2 FACH 3 FACH 4 (a) MTCH 1 MTCH 2 MTCH 3 MTCH 4 FACH 1 FACH 2 (b) S-CCPCH S-CCPCH

41 MTCHs FACHs S-CCPCHs Streaming Download Streaming + Download

43 REDUNDANT 1394 DATA BUS REDUNDANT I2C DATA BUS X X PCI DATA BUS SIO SFC P1 P1 PCI DATA BUS X X SIO P2 NVM P2 NVM P1 NVM P2 SIF P1 SIF P2 X X STM 3DB HYBRID ATTN ISI X X ATC SFG X X MCS - IN IN SITU INSTRUMENTS DIPLEXER X ANT SWITCH C O U P L E R COUPLER X SSPA I/P PWR DETECTOR DAM SUN X X MCS - REMOTE SENSING INSTRUMENTS LGA HGA O/P PWR DETECTOR GHe N2H4 SHUNT RAD X PCS X +28 V PSS-PD +28 V TO LOADS BATTERY X BCS X X PSS-VDE ACTUATION HOLD-IN NC NO LV MCS X PSE I2C DATA BUSES (2) PCAS PPS BPS X X +3.3 V PSS-PYRO PCAS S/C BPS 22 N 0.9 N x2 FOR REDUNDANT BRANCH X X2000 IN BLACK ITALICS X = INTERFACE CROSS-STRAPPED SOLAR PROBEFUNCTIONAL BLOCK DIAGRAM = power converter on slice P = power from converter on other slice

48 Coring Tool Sample Container Sleeve Lock Compliance Sample Transfer Funnel Latch Sleeve -arm Sleeve -rod

50 Ejection door

Technique Moving Target Detection (MTD) Doppler Processing Range Averaging Constant False Alarm Reduction (CFAR) Processing Increased System Bandwidth High Resolution Scan-to-Scan Averaging Clutter

magnitude of the blade returns by separating the blade spectrum into eight 125 Hz Doppler increments. Independent CFAR in each of the eight Doppler filters.

54 Technique Moving Target Detection (MTD) Doppler Processing Range Averaging Constant False Alarm Reduction (CFAR) Processing Increased System Bandwidth High Resolution Scan-to-Scan Averaging Clutter Mapping Plot and Track Filters Technique RAG Maps (Range and Azimuth Gating) Track Initiation Inhibit Sensitivity Time Control (STC) Increased radar receiver dynamic range Q Improvement Reduces the magnitude of the blade returns by separating the blade spectrum into eight 125 Hz Doppler increments. Independent CFAR in each of the eight Doppler filters. The Watchman five MHz signal bandwidth, with the resulting 30 meter resolution cell, allows detections between wind turbines. A high resolution clutter map, 30 meters in range by degrees in azimuth, controls false alarms on the individual turbines and allows detections between them. Reduces false alarms on returns that exhibit low Pd.or non-aircraft flight profiles, or fall below an operator selected ground speed. Since the CFAR/clutter map processing reduces the Pd on the turbines significantly; these filters are quite effective in further reducing the number of turbine returns that are sent to the operators. Improvement Enables unique mitigation algorithms (acceleration gates, plot suppression algorithm, low Pd algorithms, etc.) to be implemented only in wind farm areas; maintains normal performance outside of the wind farm area. Reduces false alarms and maintains Pd over wind farms. Prevents any tracks from being initiated within the wind farm area, but passes plots and allows plot association with existing tracks. Minimizes the radar sensitivity at short range in order to limit return amplitude from the wind turbine returns while not affecting target detection Reduces the impact of reflections within receiver and processor.

57 Missed Plots False Plot False Plots Missed Plots

ION PLANS POSITION LOCATION AND NAVIGATION SYMPOSIUM TECHNICAL MEETING: MAY 6 8, 2008 TUTORIALS: MAY 5 MONTEREY, CA PLANS ABSTRACTS DUE: NOVEMBER 1, 2007 PROGRAM COMMITTEE Chuck Bye, Honeywell

Penina Axelrad, University of Colorado Technical Program Co-chair THE IEEE AND THE ION ARE HOSTING PLANS TOGETHER The IEEE and the ION are pleased to announce they will equally sponsor and support

The ION s annual awards and Fellow awards, which are typically awarded during the ION s summer meeting, will be awarded during the course of PLANS 2008.

ABSTRACT SUBMISSION Please submit all abstracts via the PLANS website no later than November 1, 2007. There are two ways to submit an abstract: (1) Go to www.plansconference.

Be sure to include the paper title, the most appropriate session topic for the paper, a list of all authors and affiliations, and the primary contact author s complete mailing address, phone, fax and

Abstract title and corresponding primary author will be posted weekly on the PLANS website.

61 ION PLANS POSITION LOCATION AND NAVIGATION SYMPOSIUM TECHNICAL MEETING: MAY 6 8, 2008 TUTORIALS: MAY 5 MONTEREY, CA PLANS ABSTRACTS DUE: NOVEMBER 1, 2007 PROGRAM COMMITTEE Chuck Bye, Honeywell General Chair Wayne Soehren, Honeywell Vice Chair Dr. Penina Axelrad, University of Colorado Technical Program Co-chair THE IEEE AND THE ION ARE HOSTING PLANS TOGETHER The IEEE and the ION are pleased to announce they will equally sponsor and support the technical program and conference management of the PLANS 2008 conference. As part of the agreement, the PLANS 2008 conference will replace the ION s annual summer meeting. The ION s annual awards and Fellow awards, which are typically awarded during the ION s summer meeting, will be awarded during the course of PLANS We invite you to participate in the joint IEEE/ION meeting with exciting new opportunities for technical exchange and networking. ABSTRACT SUBMISSION Please submit all abstracts via the PLANS website no later than November 1, There are two ways to submit an abstract: (1) Go to and click on the abstract submission link; or (2) abstracts to abstracts@ion.org as a Microsoft Word or text file. Be sure to include the paper title, the most appropriate session topic for the paper, a list of all authors and affiliations, and the primary contact author s complete mailing address, phone, fax and . Abstracts should be limited to 300 words and should describe objectives, results, conclusions and the significance of your work. Abstracts will be acknowledged electronically. Abstract title and corresponding primary author will be posted weekly on the PLANS website. If your name does not appear after two weeks, please call the Institute of Navigation National Office at (703) EXHIBITS Exhibit booths are still available. See PLANS website for floor plan. AUTHOR NOTIFICATION Authors will be notified of acceptance in December and sent an electronic author s kit with presentation and publication guidelines. Papers will be published in the public domain. Classified or ITAR restricted abstracts and papers will not be accepted. All presenting authors will received an author discount on registration fees. FINAL MANUSCRIPTS Final manuscripts are due at the ION National Office by April 18, Revised papers will not be accepted after May 12, more details at Hyatt Regency Monterey, Calif.

JWST Functional Flow Diagrams and Schematic Block Diagrams

CC532 Collaborate System Design Fundamentals of Systems Engineering W6, Spring, 2012 KAIST JWST Functional Flow Diagrams and Schematic Block Diagrams 1 JWST Operational s and System Functional Breakdown