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Thrust Vector Attitude with Offset Angle
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1
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64
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March 12, 2024
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Loading Custom Gravitational Potential Models
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2
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115
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March 11, 2024
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Why can't I save the required object to the hard disk?
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4
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109
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March 6, 2024
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Ephemeris in orekit
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1
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77
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March 6, 2024
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EcksteinHechler unable to compute mean elements
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4
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80
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March 6, 2024
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Runtime of orekit software
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1
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77
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March 5, 2024
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Moon-centered rotating cr3bp frame
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3
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86
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February 24, 2024
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On the use of TEME
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8
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624
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February 23, 2024
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MSAFE files URL no longer valid
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12
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317
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February 22, 2024
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CoefficientsMatrix issue
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1
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79
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February 22, 2024
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Error when using KalmanEstimator to estimate Ephemeris
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3
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112
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February 21, 2024
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Transition matrix from 2 state vectors
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2
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112
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February 19, 2024
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Sprocket shaped propagation
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5
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82
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February 16, 2024
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Possible incorrect drag implementation in BoxAndSolarArraySpacecraft
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2
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92
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February 16, 2024
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Unexpected behavior when using withHandler((state, detector, increasing)->...) after eventsLogger.monitorDetector(detector)
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8
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78
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February 15, 2024
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Covariance frame transformation with orbital and propagation parameters
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9
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201
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February 14, 2024
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Remove additionalStateProvider
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1
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67
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February 13, 2024
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EventBasedManoeuvreTriggers unexpected behaviour with EclipseDetector
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12
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306
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February 9, 2024
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Ellipsoid Surface-Normal
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1
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65
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February 9, 2024
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KeplerianOrbit/Propagator Issue
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5
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119
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February 6, 2024
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Multiple orbits from single KeplerianOrbit
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1
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85
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February 6, 2024
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CDM XML parsing error
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11
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180
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February 2, 2024
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ImpulseManeuver and ExtremumDetector
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5
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73
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January 30, 2024
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Bug in ProfileThrustPropulsionModel?
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5
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86
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January 30, 2024
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Satellite Propagation Etude
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4
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133
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January 29, 2024
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Covariance propagation with modeled maneuvers
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7
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423
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January 26, 2024
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Maneuver thrust direction estimation
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1
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94
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January 26, 2024
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Using the the Least-Square computed covariance matrix as input in Kalman: about measurement parameters
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0
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90
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January 24, 2024
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Simple approach to trajectory calculation
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2
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83
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January 24, 2024
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Earth position does not match that of JPL Horizons
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5
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130
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January 24, 2024
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