-
1
-
-
33749251099
-
PEGASE: A DARWIN/TPF Pathfinder
-
Cambridge Univ. Press, Cambridge, England, UK, doi: 10.1017/ S1743921306009380
-
Ollivier, M., Le Duigou, J-M., Mourard, D., Absil, O., Cassaing, F., Herwats, E., et al., "PEGASE: a DARWIN/TPF Pathfinder," Proceedings of the International Astronomical Union, Cambridge Univ. Press, Cambridge, England, UK, 2005, pp. 241-246. doi: 10.1017/S1743921306009380
-
(2005)
Proceedings of the International Astronomical Union
, pp. 241-246
-
-
Ollivier, M.1
Le Duigou, J.-M.2
Mourard, D.3
Absil, O.4
Cassaing, F.5
Herwats, E.6
-
2
-
-
72149087383
-
LISA: Probing the universe with gravitationalwaves
-
"LISA: Probing the Universe with GravitationalWaves," LISA Mission Science Office LISA-LIST-RP-436, Vol. 1, 2007, pp. 1-117.
-
(2007)
LISA Mission Science Office LISA-LIST-RP-436
, vol.1
, pp. 1-117
-
-
-
3
-
-
15944427552
-
TanDEM-X: ATerraSAR-X add-on satellite for single-pass SAR interferometry
-
Institute of Electrical and Electronics Engineers, New York, Sept. doi:10.1109/IGARSS.2004.1368578
-
Moreira, A., et al., "TanDEM-X: ATerraSAR-X Add-On Satellite for Single-Pass SAR Interferometry," Geoscience & Remote Sensing Symposium, Vol. 2, Institute of Electrical and Electronics Engineers, New York, Sept. 2004, pp. 1000-1003. doi:10.1109/IGARSS.2004.1368578
-
(2004)
Geoscience & Remote Sensing Symposium
, vol.2
, pp. 1000-1003
-
-
Moreira, A.1
-
4
-
-
3543124806
-
The gravity recovery and climate experiment: Mission overview and early results
-
DOI 10.1029/2004GL019920
-
Tapley, B. D., Bettadpur, S.,Watkins, M., and Reigber, C., "The Gravity Recovery and Climate Experiment: Mission Overview and Early Results," Geophysical Research Letters, Vol. 31, 2004, L09607. doi:10.1029/2004GL019920 (Pubitemid 39026633)
-
(2004)
Geophysical Research Letters
, vol.31
, Issue.9
-
-
Tapley, B.D.1
Bettadpur, S.2
Watkins, M.3
Reigber, C.4
-
5
-
-
72149086333
-
-
DLR, TN 05-08, Cologne, Germany
-
D'Amico, S., "Relative Orbital Elements as Integration Constants of the Hill's Equations," DLR, TN 05-08, Cologne, Germany, 2005.
-
(2005)
Relative Orbital Elements as Integration Constants of the Hill's Equations
-
-
D'Amico, S.1
-
6
-
-
0001422127
-
Terminal guidance system for satellite rendezvous
-
Clohessy, W. H., and Wiltshire, R. S., "Terminal Guidance System for Satellite Rendezvous," Journal of the Aerospace Sciences, Vol. 27, 1960, pp. 653-658.
-
(1960)
Journal of the Aerospace Sciences
, vol.27
, pp. 653-658
-
-
Clohessy, W.H.1
Wiltshire, R.S.2
-
7
-
-
0002311236
-
Researches in the lunar theory
-
doi:10.2307/2369430
-
Hill, G. W., "Researches in the Lunar Theory," American Journal of Mathematics, Vol. 1, 1878, pp. 5-26. doi:10.2307/2369430
-
(1878)
American Journal of Mathematics
, vol.1
, pp. 5-26
-
-
Hill, G.W.1
-
8
-
-
0035269743
-
Formation flying design and evolution
-
doi:10.2514/2.3681
-
Sabol, C., Burns, R., and McLaughlin, C. A., "Formation Flying Design and Evolution," Journal of Spacecraft and Rockets, Vol. 38, No. 2, 2001, pp. 270-278. doi:10.2514/2.3681
-
(2001)
Journal of Spacecraft and Rockets
, vol.38
, Issue.2
, pp. 270-278
-
-
Sabol, C.1
Burns, R.2
McLaughlin, C.A.3
-
9
-
-
0036857921
-
2 model for satellite formation flight
-
doi:10.2514/2.4986
-
2 Model for Satellite Formation Flight," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 6, 2002, pp. 1073-1080. doi:10.2514/2.4986
-
(2002)
Journal of Guidance, Control, and Dynamics
, vol.25
, Issue.6
, pp. 1073-1080
-
-
Schweighart, S.1
Sedwick, R.2
-
10
-
-
0036157296
-
Relative dynamics and control of spacecraft formations in eccentric orbits
-
doi:10.2514/2.4874
-
Inalhan, G., Tillerson, M., and How, J. P., "Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 1, 2002, pp. 48-60. doi:10.2514/2.4874
-
(2002)
Journal of Guidance, Control, and Dynamics
, vol.25
, Issue.1
, pp. 48-60
-
-
Inalhan, G.1
Tillerson, M.2
How, J.P.3
-
13
-
-
4944250210
-
Relative orbit geometry through classical orbit element differences
-
Sept.-Oct. doi:10.2514/1.12595
-
Schaub, H., "Relative Orbit Geometry Through Classical Orbit Element Differences," Journal of Guidance, Control, and Dynamics, Vol. 27, No. 5, Sept.-Oct. 2004, pp. 839-848. doi:10.2514/1.12595
-
(2004)
Journal of Guidance, Control, and Dynamics
, vol.27
, Issue.5
, pp. 839-848
-
-
Schaub, H.1
-
14
-
-
33744774006
-
Colocation strategy and collision avoidance for the geostationary satellites at 19 degrees west
-
Eckstein, M. C., Rajasingh, C. K., and Blumer, P., "Colocation Strategy and Collision Avoidance for the Geostationary Satellites at 19 degrees west," International Symposium on Space Flight Dynamics, 1989.
-
(1989)
International Symposium on Space Flight Dynamics
-
-
Eckstein, M.C.1
Rajasingh, C.K.2
Blumer, P.3
-
15
-
-
33749537054
-
E/I-vector separation for safe switching of the GRACE formation
-
DOI 10.1016/j.ast.2006.04.001, PII S1270963806000472
-
Montenbruck, O., Kirschner, M., D'Amico, S., and Bettadpur, S., "E/IVector Separation for Safe Switching of the GRACE Formation," Aerospace Science and Technology, Vol. 10, 2006, pp. 628-635. doi:10.1016/j.ast.2006.04.001 (Pubitemid 44528306)
-
(2006)
Aerospace Science and Technology
, vol.10
, Issue.7
, pp. 628-635
-
-
Montenbruck, O.1
Kirschner, M.2
D'Amico, S.3
Bettadpur, S.4
-
16
-
-
33744765243
-
Proximity operations of formation-flying spacecraft, using an eccentricity/inclination vector separation
-
May-June doi:10.2514/1.15114
-
D'Amico, S., and Montenbruck, O., "Proximity Operations of Formation-Flying Spacecraft, Using an Eccentricity/Inclination Vector Separation," Journal of Guidance, Control, and Dynamics, Vol. 29, No. 3, May-June 2006, pp. 554-563. doi:10.2514/1.15114
-
(2006)
Journal of Guidance, Control, and Dynamics
, vol.29
, Issue.3
, pp. 554-563
-
-
D'Amico, S.1
Montenbruck, O.2
-
17
-
-
33845798472
-
-
AIAA Paper 2006-6067, Aug.
-
D'Amico, S., Gill, E., and Montenbruck, O., "Relative Orbit Control Design for the PRISMA Formation Flying Mission,"AIAA Paper 2006-6067, Aug. 2006.
-
(2006)
Relative Orbit Control Design for the PRISMA Formation Flying Mission
-
-
D'Amico, S.1
Gill, E.2
Montenbruck, O.3
-
18
-
-
3843075181
-
Tight formation flying for an along-track SAR interferometer
-
doi:10.1016/j.actaastro.2004.05.044
-
Gill, E., and Runge, H., "Tight Formation Flying for an Along-Track SAR interferometer," Acta Astronautica, Vol. 55, No. 3-9, 2004, pp. 473-485. doi:10.1016/j.actaastro.2004.05.044
-
(2004)
Acta Astronautica
, vol.55
, Issue.3-9
, pp. 473-485
-
-
Gill, E.1
Runge, H.2
-
20
-
-
23844449566
-
Orbit control techniques for low earth orbiting (LEO) satellites
-
edited by J. P. Carrou, Cepadues-Editions, Toulouse, France
-
Micheau, P., "Orbit Control Techniques for Low Earth Orbiting (LEO) Satellites," Spaceflight Dynamics, edited by J. P. Carrou, Cepadues-Editions, Toulouse, France, 1995.
-
(1995)
Spaceflight Dynamics
-
-
Micheau, P.1
-
21
-
-
0035394681
-
Impulsive feedback control to establish specific mean orbit elements of spacecraft formations
-
doi:10.2514/2.4774
-
Schaub, H., and Alfriend, K. T., "Impulsive Feedback Control to Establish Specific Mean Orbit Elements of Spacecraft Formations," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 4, 2001, pp. 739-745. doi:10.2514/2.4774
-
(2001)
Journal of Guidance, Control, and Dynamics
, vol.24
, Issue.4
, pp. 739-745
-
-
Schaub, H.1
Alfriend, K.T.2
-
22
-
-
15744378998
-
Formation establishment and reconfiguration using impulsive control
-
March-April, doi:10.2514/1.6687
-
Vaddi, S. S., Alfriend, K. T.,Vadali, S. R., and Sengupta, P., "Formation Establishment and Reconfiguration Using Impulsive Control," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 2, March-April 2005, pp. 262-268. doi:10.2514/1.6687
-
(2005)
Journal of Guidance, Control, and Dynamics
, vol.28
, Issue.2
, pp. 262-268
-
-
Vaddi, S.S.1
Alfriend, K.T.2
Vadali, S.R.3
Sengupta, P.4
-
23
-
-
15744362855
-
-
American Astronautical Society Paper 03-652, Aug.
-
Alfriend, K. T.,Vaddi, S. S., and Lovell, T. A., "Formation Maintenance for Low Earth Near Circular Orbits," American Astronautical Society Paper 03-652, Aug. 2003.
-
(2003)
Formation Maintenance for Low Earth Near Circular Orbits
-
-
Alfriend, K.T.1
Vaddi, S.S.2
Lovell, T.A.3
-
24
-
-
33845810401
-
-
AIAA Paper 1999-4265, July-Aug.
-
Vadali, S. R., Schaub, H., and Alfriend, K. T., "Initial Conditions and Fuel Optimal Control for Formation Flying of Satellites," AIAA Paper 1999-4265, July-Aug. 1999.
-
(1999)
Initial Conditions and Fuel Optimal Control for Formation Flying of Satellites
-
-
Vadali, S.R.1
Schaub, H.2
Alfriend, K.T.3
-
25
-
-
72149116376
-
The mosaicgnss receiver family, orbit and attitude determination in various orbits
-
Mittnacht, M., Gottzein, E., Hartrampf, M., Heim, J., and Krauss, P. A., "The MosaicGNSS Receiver Family, Orbit and Attitude Determination in Various Orbits," European Space Research and Technology Centre Paper 13.4, 2004.
-
(2004)
European Space Research and Technology Centre Paper
, vol.13
, Issue.4
-
-
Mittnacht, M.1
Gottzein, E.2
Hartrampf, M.3
Heim, J.4
Krauss, P.A.5
-
26
-
-
0001573933
-
Solution of the problem of artificial satellite theory without drag
-
doi:10.1086/107958
-
Brouwer, D., "Solution of the Problem of Artificial Satellite Theory Without Drag," Astronomical Journal, Vol. 64, No. 1274, 1959, p. 378. doi:10.1086/107958
-
(1959)
Astronomical Journal
, vol.64
, Issue.1274
, pp. 378
-
-
Brouwer, D.1
-
27
-
-
85024423711
-
New results in linear filtering and prediction theory
-
Kalman, R. E., and Bucy, R. S., "New Results in Linear Filtering and Prediction Theory," Journal of Basic Engineering, Vol. 83, 1961, pp. 95-108.
-
(1961)
Journal of Basic Engineering
, vol.83
, pp. 95-108
-
-
Kalman, R.E.1
Bucy, R.S.2
-
28
-
-
0029373108
-
GRAFCET: A powerful tool for specification of logic controllers
-
Sep. doi:10.1109/87.406973
-
David, R., "GRAFCET: A Powerful Tool for Specification of Logic Controllers," IEEE Transactions on Control Systems Technology, Vol. 3, No. 3, Sep. 1995, pp. 253-268. doi:10.1109/87.406973
-
(1995)
IEEE Transactions on Control Systems Technology
, vol.3
, Issue.3
, pp. 253-268
-
-
David, R.1
-
29
-
-
8344263776
-
A miniature gps receiver for precise orbit determination of the SUNSAT2004 micro-satellite
-
Jan.
-
Montenbruck, O., Nortier, B., and Mostert, S., "A Miniature GPS Receiver for Precise Orbit Determination of the SUNSAT2004 Micro-Satellite, " ION National Technical Meeting, Jan. 2004, pp. 636-642.
-
(2004)
ION National Technical Meeting
, pp. 636-642
-
-
Montenbruck, O.1
Nortier, B.2
Mostert, S.3
-
30
-
-
0012698396
-
-
Gaisler Research, Gothenburg, Sweden
-
Gaisler, J., "The LEON Processor User's Manual," Gaisler Research, Gothenburg, Sweden, 2001, pp. 235-237.
-
(2001)
The LEON Processor User's Manual
, pp. 235-237
-
-
Gaisler, J.1
|