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DTIC ADA1045426: Flight Trajectory Control Investigation |
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by Defense Technical Information Center |
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Optimal control algorithms for four-dimensional guidance |
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of a transport aircraft were investigated for |
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feasibility. Cost function constraints on the optimal |
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reference path generator appeared impossible to achieve |
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and the optimal guidance algorithms do not achieve |
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significant performance improvement without excessive |
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increases in sophistication and cost of the onboard |
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avionics computer. A modularized existing Mission |
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Management system allows a three-phase flight test plan |
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to demonstrate the operational capability of the existing |
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classical integrated flight trajectory control |
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algorithms. (Author) |
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Date Published: 2020-04-28 01:33:05 |
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Identifier: DTIC_ADA1045426 |
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Item Size: 95146356 |
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Language: english |
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Media Type: texts |
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# Topics |
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DTIC Archive; Bird, M ; LEAR SIEGLER ... |
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# Uploaded by |
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@chris85 |
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