I remember some of the history of IBM's smallest program:

http://en.m.wikipedia.org/wiki/IEFBR14

In addition to the changes my friend John Pershing mentions, I recall bug 
reports due to inadequate comments, and because the number of changes per line 
of code was high, IEFBR14 was high on a list of modules that needed a rewrite...

Software work helps one with humility...

73 de Dick, K6KR


> On Jan 17, 2015, at 14:30, KENT TRIMBLE <[email protected]> wrote:
> 
> Facts can also be factual.
> 
> Kent  K9ZTV
> 
> 
> /On November 10, 1999, the Mars Climate Orbiter Mishap Investigation Board 
> released a Phase I report, detailing the suspected issues encountered with 
> the loss of the spacecraft. Previously, on September 8, 1999, Trajectory 
> Correction Maneuver-4 was computed and then executed on September 15, 1999. 
> It was intended to place the spacecraft at an optimal position for an orbital 
> insertion maneuver that would bring the spacecraft around Mars at an altitude 
> of 226 kilometers on September 23, 1999. However, during the week between 
> TCM-4 and the orbital insertion maneuver, the navigation team indicated the 
> altitude may be much lower than intended at 150 to 170 kilometers. 
> Twenty-four hours prior to orbital insertion, calculations placed the orbiter 
> at an altitude of 110 kilometers; 80 kilometers is the minimum altitude that 
> Mars Climate Orbiter was thought to be capable of surviving during this 
> maneuver. Post-failure calculations showed that the spacecraft was on a 
> trajectory that w
 ould have taken the orbiter within 57 kilometers of the surface, where the 
spacecraft likely disintegrated because of atmospheric stresses. /
> 
> /_The primary cause of this discrepancy was that one piece of ground software 
> supplied by _Lockheed Martin 
> <http://en.wikipedia.org/wiki/Lockheed_Martin>_produced results in a _United 
> States customary unit 
> <http://en.wikipedia.org/wiki/United_States_customary_units>_("American"), 
> contrary to its Software Interface Specification (SIS), while a second 
> system, supplied by _NASA <http://en.wikipedia.org/wiki/NASA>_, that used 
> those results expected them to be in metric units, in accord with the SIS. 
> _Software that calculated the total impulse produced by thruster firings 
> calculated results in pound-seconds. The trajectory calculation used these 
> results to correct the predicted position of the spacecraft for the effects 
> of thruster firings. This software expected its inputs to be in 
> newton-seconds.^[16] 
> <http://en.wikipedia.org/wiki/Mars_Climate_Orbiter#cite_note-Mishap-17> /
> 
> //
> 
> /The discrepancy between calculated and measured position, resulting in the 
> discrepancy between desired and actual orbit insertion altitude, had been 
> noticed earlier by at least two navigators, whose concerns were dismissed. A 
> meeting of trajectory software engineers, trajectory software operators 
> (navigators), propulsion engineers, and managers, was convened to consider 
> the possibility of executing Trajectory Correction Maneuver-5, which was in 
> the schedule. Attendees of the meeting recall an agreement to conduct TCM-5, 
> but it was ultimately not done./
> 
> 
> 
>> On 1/17/2015 1:41 PM, Lynn W. Taylor, WB6UUT wrote:
>> Good quip, but it doesn't agree with the findings of the Mars Climate 
>> Orbiter Mishap Investigation Board.
>> 
>> Facts can be so inconvenient.
>> 
>>> On 1/17/2015 11:15 AM, KENT TRIMBLE wrote:
>>> Good quips always sail over at least one person's head.
>>> 
>>> K9ZTV 
>> 
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