TPF-I SWG Report - Exoplanet Exploration Program - NASA

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A PPENDIX C References Cohen, S., and Hindmarsh, A., “CVODE, a Stiff/Nonstiff ODE Solver in C,” Computers in Physics 10 (2), 138–143 (1996). Jain, A., and Rodriguez, G., “Recursive Flexible Multibody System Dynamics Using Spatial Operators,” Journal of Guidance, Control and Dynamics 15, 1453–1466 (1992). Lay, O. P., and Blackwood, G. H., “Formation-Flying Interferometry,” Interferometry in Space, edited by M. Shao, Proc. SPIE 4852, 481–491 (2003). Lurie, B., “Multi-Mode Synchronized Control for Formation Flying Interferometer ,” AIAA Guidance, Navigation, and Control Conference, Austin, TX, 11–14 August 2003, paper 5365 (2003). Martin, B. J., and Sohl, G. A., “HYDRA: High-Speed Simulation Architecture for Precision Spacecraft Formation Simulation,” AIAA Modeling and Simulation Technologies Conf., Austin, TX, 11–14 August, paper 5380 (2003). Ploen, S. R., Scharf, D. P., Hadaegh, F. Y., and Bikdash, M., “Guaranteed Initialization of Distributed Spacecraft Formations,” Journal of the Astronautical Sciences 52 (4), 495–515 (2004). Scharf, D. P., Acikmese, A. B., Ploen, S. R., and Hadaegh, F. Y., “A Direct Solution for Fuel-Optimal Reactive Collision Avoidance of Collaborating Spacecraft,” American Control Conference, Minneapolis, MN, 14–16 June (2006). Scharf, D. P., Hadaegh. F. Y. and Kang, B. H., “On the Validity of the Double Integrator Approximation in Deep Space Formation Flying,” First International Symposium on Formation Flying Missions and Technologies, Centre National d’Etudes Spatiales, Toulouse, France, (Oct. 29–30, 2002). Scharf, D. P., Hadaegh, F. Y., Rahman, Z. R., Shields, J. H., Singh, G., and Wette, M. R., “An Overview of the Formation and Attitude Control System for the Terrestrial Planet Finder Formation Flying Interferometer,” 2nd International Symposium on Formation Flying Missions and Technologies, Washington, D.C. (September 2004). Scharf, D. P., Ploen, S. R., Hadaegh, F. Y., and Sohl, G. A., “Guaranteed Spatial Initialization of Distributed Spacecraft Formations,” AIAA Guidance, Navigation and Control Conference, Providence, RI, 16–19 August 2004, paper 4893 (2004). Singh, G., and Hadaegh, F. Y., “Collision Avoidance Guidance for Formation-Flying Applications,” AIAA Guidance, Navigation, and Control Conference, Montreal, PQ, 6–9 August, paper 4088 (2001). Sohl, G. A., Udomkesmalee, S., and Kellogg, J. L., “Distributed Simulation for Formation Flying Applications,” AIAA Modeling and Simulation Technologies Conference, San Francisco, CA, 15–18 August 2005, paper 6494 (2005). 188
A C R O N Y M S Appendix D Acronyms ACS AdN ADP AFF AGB AgCl AGN ALMA ANT AO Ar ARR ASO ATLO ATS AU BC BL BOL Attitude Control System Adaptive Nuller Testbed acceleration data processing (algorithm) autonomous formation flying asymptotic giant branch silver chloride Active Galactic Nucleus (or Nuclei) Atacama Large Millimeter Array Achromatic Nulling Testbed adaptive optics argon Assembly Readiness Review Astronomical Search for Origins Assembly, Test, and Launch Operations absolute translation system astronomical unit; approximately the mean distance between the Earth and the Sun beam combiner baseline beginning of life CAC collision-avoidance constraint CCD charged couple device CCl 2 F 2 freon 13 CCL 3 F freon 12 CDR Critical Design Review CG center-of-gravity CH 3 Cl methyl chloride CH 4 methane CIRS Composite Infrared Spectrometer (on the Cassini mission) CM center of mass CMC center-of-mass to center-of-mass (relative position) CNES Centre National d’Etudes Spatiales CO 2 carbon dioxide CoRoT Convection Rotation and Planetary Transits (CNES, France) CTE coefficient of thermal expansion DAC DARTS degenerate Angel cross Dynamics Algorithms for Real-Time Simulation 189
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JPL Publication 07-1 Terrestrial Pl
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Abstract Over the past two years, t
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Acknowledgements Twenty-two represe
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Table of Contents 1 Introduction...
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4.8.3 Post-Nulling Calibration.....
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6.4.5 Double Fourier Interferometry
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I NTRODUCTION 1 Introduction Over 2
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I NTRODUCTION et al. 2004), and res
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I NTRODUCTION Standard Interferomet
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I NTRODUCTION 1.4 References Angel,
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C HAPTER 2 0.7 to 1.5 AU scaled by
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C HAPTER 2 Table 2-2. Illustrative
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C HAPTER 2 Classical interferometry
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C HAPTER 2 trivial in the absence o
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C HAPTER 2 Figure 2-3. Simulated mi
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C HAPTER 2 would be in atmospheres
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C HAPTER 2 Figure 2-6. The mid-infr
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C HAPTER 2 Lines of constant stella
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C HAPTER 2 presence of zodiacal clo
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C HAPTER 2 S EZ 2π ∫ θ max ∫
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C HAPTER 2 Figure 2-11. Observation
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C HAPTER 2 Figure 2-12. Models of t
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C HAPTER 2 Beichman, C. A., Fridlun
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C HAPTER 2 2.7.4 Suitable Targets E
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C HAPTER 2 Reach, W. T., Franz, B.
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C HAPTER 3 3.1.1 Darwin/TPF-I Prope
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C HAPTER 3 clouds or an OB associat
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C HAPTER 3 Figure 3-3. Three possib
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C HAPTER 3 the circumstellar disk,
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C HAPTER 3 Figure 3-6. (Left panel)
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C HAPTER 3 Continuum interferometry
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C HAPTER 3 Figure 3-9: Simulated im
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C HAPTER 3 3.3 Conclusions Darwin/T
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C HAPTER 3 Nguyen, H. T., Kallivaya
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D ESIGN AND A R C H I T E C T U R E
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C HAPTER 5 Heavy launch vehicle. Th
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C HAPTER 5 5.3.2 Combiner Spacecraf
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C HAPTER 5 5.3.5 Beam Transfer betw
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C HAPTER 5 Figure 5-8. Control sche
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C HAPTER 5 Figure 5-9. First sectio
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C HAPTER 5 Figure 5-9 shows the fir
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C HAPTER 5 5.4.4 Shear Metrology Sh
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C HAPTER 5 Figure 5-15. TPF-I Fligh
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C HAPTER 5 secondary mirror along t
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C HAPTER 5 a) c) b) d) IWA = 43 mas
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C HAPTER 5 planets found. Figure 5-
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C HAPTER 5 30 25 5 M earth 3 M eart
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C HAPTER 5 5.8.4 Angular Resolution
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C HAPTER 5 Table 5-3. Angular Resol
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C HAPTER 5 The optimization works b
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T E C H N O L O G Y R OADMAP FOR TP
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Page 151 and 152: T E C H N O L O G Y R OADMAP FOR TP
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Page 183 and 184: T E C H N O L O G Y A DVISORY C O M
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Page 200 and 201: A PPENDIX C The “true” time of
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Page 208 and 209: A PPENDIX E Appendix E TPF-I Review
Page 210 and 211: A PPENDIX F Alice Quillen, Universi
Page 212: A PPENDIX F Figure 3-1 - Original f
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