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It is often stated that Neil took manual control of the LM to fly past
a bad landing site. But wasn't it planned that the CDR would take over at some point? |
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The LM had a full "autoland" but no CDR ever used it; they all went into
the semi-auto landing mode. No-one ever used the full manual landing mode. On 25/09/2012 11:14, Jan Philips wrote: It is often stated that Neil took manual control of the LM to fly past a bad landing site. But wasn't it planned that the CDR would take over at some point? |
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On 25/09/2012 02:14, Jan Philips wrote:
It is often stated that Neil took manual control of the LM to fly past a bad landing site. But wasn't it planned that the CDR would take over at some point? The LMGC (Lunar Module Guidance Computer) controlled the Powered Descent via five main programs (P63, P64, P65, P66 & P68). In theory these could have guided the LM to a safe touchdown. However, the Luminary software package could not determine whether the designated landing site was suitable, therefore the option to take over 'manual' control was built in. In practice no CDR would ever let the computer fly the landing. The whole Powered Descent was divided into three phases - the Braking Phase, which began with PDI and was controlled by P63; the Approach Phase (P64) which delivered the LM to around 1000 feet at which point the LM was rotated so that the crew could finally see the landing site ('Pitchover'); and the Landing Phase (P65). P65 was the automatic landing program and the CDR had the option to take control by requesting P66. P66 continued to maintain some aspects of the descent, but the CDR took control of attitude and rate of descent. P68 was the landing confirmation program which was loaded after shutdown. I'm not sure about P67 - it appears to have written to control the LM if the designated landing site had been passed, presumably leading to an abort. There are very detailed and highly technical documents about the Luminary software he http://www.ibiblio.org/apollo/Luminary.html Note: Early versions of Luminary were named Sunburst & Sundance. MIT was responsible for the development and coding. The primary author of the P60 programs was Don Eyles. -- Brian W Lawrence Wantage Oxfordshire |
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In Brian Lawrence writes:
On 25/09/2012 02:14, Jan Philips wrote: It is often stated that Neil took manual control of the LM to fly past a bad landing site. But wasn't it planned that the CDR would take over at some point? The LMGC (Lunar Module Guidance Computer) controlled the Powered Descent via five main programs (P63, P64, P65, P66 & P68). In theory these could have guided the LM to a safe touchdown. However, the Luminary software package could not determine whether the designated landing site was suitable, therefore the option to take over 'manual' control was built in. In practice no CDR would ever let the computer fly the landing. James Lovell claimed, around the time the movie came out, that he intended to let the computer fly Aquarius to touchdown, barring some extraordinary circumstance (such as the discovery of a small rock field in the last minutes). Granted, he's also the person who could claim that. -- http://nebusresearch.wordpress.com/ Joseph Nebus Current Entry: My Problem With 7 http://wp.me/p1RYhY-ju ------------------------------------------------------------------------------ |
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On Mon, 24 Sep 2012 21:14:49 -0400, Jan Philips
wrote: It is often stated that Neil took manual control of the LM to fly past a bad landing site. But wasn't it planned that the CDR would take over at some point? Thank you for the informative replies. |
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