System analysis is an essential technical discipline for the modern design of spacecraft and their associated missions. Specifically, system analysis is a powerful aid in identifying and prioritizing the required technologies needed for mission and/or vehicle development efforts. Maturation of intelligent systems technologies, and their incorporation into spacecraft systems, are dictating the development of new analysis tools, and incorporation of such tools into existing system analysis methodologies, in order to fully capture the trade-offs of autonomy on vehicle and mission success. A 'system analysis of autonomy' methodology will be outlined and applied to a set of notional human-rated lunar/Mars lander missions toward answering these questions: 1. what is the optimum level of vehicle autonomy and intelligence required. and 2. what are the specific attributes of an autonomous system implementation essential for a given surface lander mission/application in order to maximize mission success. Future human-rated lunar/Mars landers, though nominally under the control of their crew, will, nonetheless, be highly automated systems. These automated systems will range from mission/flight control functions, to vehicle health monitoring and prognostication, to life-support and other 'housekeeping' functions. The optimum degree of autonomy afforded to these spacecraft systems/functions has profound implications from an exploration system architecture standpoint.
System Analysis Applied to Autonomy: Application to Human-Rated Lunar/Mars Landers
2006
23 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Manned Spacecraft , Manned spacecraft , Autonomy , Systems analysis , Flight control , Landing modules , Spacecraft design , Systems engineering , Spacecraft control , Mars missions , Trajectory control , Lunar landing , Manned mars missions , Space navigation , Mission planning
AIAA-2006-7516 System Analysis Applied to Autonomy: Application to Human-Rated Lunar/Mars Landers
British Library Conference Proceedings | 2006
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