Publikationsdatum:
2019-07-13
Beschreibung:
Propellant-optimal trajectories, relative sensors and navigation, and docking/capture mechanisms are rendezvous disciplines that receive much attention in the technical literature. However, other areas must be considered. These include absolute navigation, maneuver targeting, attitude control, power generation, software development and verification, redundancy management, thermal control, avionics integration, robotics, communications, lighting, human factors, crew timeline, procedure development, orbital debris risk mitigation, structures, plume impingement, logistics, and in some cases extravehicular activity. While current and future spaceflight programs will introduce new technologies and operations concepts, the complexity of integrating multiple systems on multiple spacecraft will remain. The systems integration task may become more difficult as increasingly complex software is used to meet current and future automation, autonomy, and robotic operation requirements.
Schlagwort(e):
Spacecraft Design, Testing and Performance
Materialart:
JSC-17709
,
AAS 09-065
,
2009 AAS GN&C Conference; Jan 30, 2009 - Feb 04, 2009; Virginia; United States
Format:
application/pdf
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