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NASA NTRS · 19670060447

A manually retargeted automatic descent and landing system for LM.

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Abstract

Manual steering problem and function of lunar module /LM/ manual hybrid guidance system, with automatic guidance system produced trajectory

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MANUAL CONTROL TRAJECTORY CONTROL APPROACH CONTROL GUIDANCE (MOTION)LUNAR LANDING MODULE

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Klumpp, A. R.. 1967-09-01. A manually retargeted automatic descent and landing system for LM.. https://ntrs.nasa.gov/citations/19670060447

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