Dream Chaser On-Orbit Operations: Preliminary Trajectory Design and Analysis
Author:
Affiliation:
1. Draper Laboratory
2. Sierra Nevada Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6654
Reference6 articles.
1. Trigger Angle Targeting for Orbital Rendezvous
2. Linear Covariance Techniques for Orbital Rendezvous Analysis and Autonomous Onboard Mission Planning
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1. Mars Entry Guidance and Navigation Analysis Using Linear Covariance Techniques for the Safe and Precise Landing -- Integrated Capabilities Evolution (SPLICE) Project;AIAA Scitech 2020 Forum;2020-01-05
2. Linear Covariance Analysis Techniques to Generate Navigation and Sensor Requirements for the Safe and Precise Landing Integrated Capabilities Evolution (SPLICE) Project;AIAA Scitech 2019 Forum;2019-01-06
3. Automated Derivation and Verification of Navigation Requirements for On-Orbit Rendezvous;AIAA Guidance, Navigation, and Control (GNC) Conference;2013-08-15
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