FM/Assistant ChiefMAR 27 196767-FM1-25FM/Deputy ChiefNone
This action item was given MIT by FCD. We stopped it.
Provide criteria for checking the “usability of guidance equations and the navigation vector”. If practical, it would be desirable to fly a “hands off” mission, but it was recognized that for degra- dations in the state vector (or trajectory) it would eventually be- come necessary to update the time of a burn, its targeting, or both (plus perhaps a state vector).
But it needs to be done… Will you get someone to do it? GPB, I guess.
- Jul 18, 1968 – No 15 minute constraint for Lunar Ascent Guidance (3.3σ)
1967_tindallgrams.pdf
