The application of concurrentengineering approach to the design of a large flexible space structure is discussed. A full system model using bond graphs incorporating orbital and ballistic dynamics, controls, optics, ...
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The application of concurrentengineering approach to the design of a large flexible space structure is discussed. A full system model using bond graphs incorporating orbital and ballistic dynamics, controls, optics, and vibrational analyses is developed. design of experiment techniques is used to analyze the entire system and determine the optimum set of design parameters. The objective of the design effort involved the simultaneous design of the control algorithm, structural characteristics, and optical geometry. The system size and mass were limited by current space shuttle capabilities. The satellite was required to track the missile plume of an ICBM with minimum line-of-site error, and transmit the position data to earth.< >
Proceedings incorporates 43 papers. These are arranged into six sessions dealing with the following major topics: assembly methods and materials for optical systems;advanced optical manufacturing and testing;optical d...
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ISBN:
(纸本)0819409251
Proceedings incorporates 43 papers. These are arranged into six sessions dealing with the following major topics: assembly methods and materials for optical systems;advanced optical manufacturing and testing;opticaldesign and engineering;optical fabrication and testing;as well as contemporary optical systems and devices.
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