Re: [Elecraft] Buggy software OT

2015-01-18 Thread Eric Swartz - WA6HHQ, Elecraft
Guys, time to end this Ot thread. In the future, please do not wait for me to 
step in. I can't watch the list continually if you also expect us to ship 
products to you quickly ;-)

Self moderate after an OT thread has gone past 5-10 postings.

Eric
Elecraft list moderator etc.
elecraft.com
_..._



 On Jan 17, 2015, at 7:32 PM, Guy Olinger K2AV k2av@gmail.com wrote:
 
 On Sat, Jan 17, 2015 at 4:40 PM, Dick Dievendorff d...@elecraft.com wrote:
 
 Software work helps one with humility...
 
 
 If software developing hasn't already beaten one into mumbling and slurring
 of words without any assistance from the juice.
 
 I remember so many days going home with a splitting headache, literal pain.
 
 73, Guy.
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Re: [Elecraft] Buggy software OT

2015-01-17 Thread KENT TRIMBLE

Good quips always sail over at least one person's head.

K9ZTV


On 1/17/2015 1:09 PM, Lynn W. Taylor, WB6UUT wrote:
Totally different.  This was not flight software -- and it wasn't 
all software, either.


I'm sure we're over the OT limit, but it's really difficult for those 
of us who did this for a living to read posts from people who don't 
know what it takes to actually do.


On 1/17/2015 10:54 AM, KENT TRIMBLE wrote:
Otherwise known as the strategy perfected by JPL in 1998 for the Mars 
Climate Orbiter . . . one in English units and the other in metric.


K9ZTV 


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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Dale Putnam
Is that software for a single... or a pair of trotters? 
Or... is it actually for a surrey?  Fringed?
So many questions... so few answers..

;-O

Have a great day, 
 
 
--...   ...--
Dale - WC7S in Wy
 
 


  
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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Bill Gerth
Then, would you be so kind as to enlighten us?

73,
BILL
W4RK

On Jan 17, 2015, at 1:41 PM, Lynn W. Taylor, WB6UUT 
k...@coldrockshotbrooms.com 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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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Lynn W. Taylor, WB6UUT
This needs to stop here, but since Kent is saying that I don't 
understand, I'm going to reply.  Once.


We were talking about how a hypothetical airliner control system would 
have two different programs, written by different groups, running 
parallel, with either program capable of flying the plane.  Part of the 
flight system could crash that the pilots and passengers would not 
notice.  Airplanes in flight have to have controls that work in 
milliseconds without a glitch.


With MRO, we have Lockheed software doing navigation, but not flying 
the spacecraft.  JPL software flew the spacecraft, but did not 
navigate.  If JPL did their own redundant navigation, the error would 
have been caught.


It's not like they didn't have time, there was a week between the 
calculation and the burn.


The facts in the Wikipedia article are correct, it just doesn't describe 
a system that has any redundancy.


I will not comment further on this topic on list.  We're way over the 
limit on off-topic posts.


73 -- Lynn

On 1/17/2015 12:30 PM, KENT TRIMBLE wrote:

Facts can also be factual.

Kent  K9ZTV

/snip/

/_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 /




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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Lynn W. Taylor, WB6UUT
The Airbus software won't let the pilot do anything that might break the 
airplane.  The Boeing software doesn't have the same limits.


I believe there are accidents attributed to both.

For critical systems, there are often two different programs, written by 
different groups of programmers, either of which can fly the 
airplane.  The assumption is that they'll have different bugs.


On 1/17/2015 12:40 AM, Fred Townsend wrote:

I think there is a big difference in flight software. In Boeing airplanes
the pilot is assisted by software. In Airbuses the pilot is allowed to fly
the airplane if the software thinks he/she is qualified. There has been at
least one airbus crash blamed on software and several other questionable
crashes.


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Re: [Elecraft] Buggy software OT

2015-01-17 Thread KENT TRIMBLE

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 would 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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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Dick Dievendorff
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 k9...@socket.net 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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 Checked by AVG - www.avg.com
 Version: 2015.0.5645 / Virus Database: 4260/8946 - Release Date: 01/17/15
 
 
 
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Re: [Elecraft] Buggy software OT

2015-01-17 Thread KENT TRIMBLE
Otherwise known as the strategy perfected by JPL in 1998 for the Mars 
Climate Orbiter . . . one in English units and the other in metric.


K9ZTV


On 1/17/2015 12:13 PM, someone wrote:
For critical systems, there are often two different programs, written 
by different groups of programmers, either of which can fly the 
airplane.  The assumption is that they'll have different bugs.


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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Lynn W. Taylor, WB6UUT
Totally different.  This was not flight software -- and it wasn't all 
software, either.


I'm sure we're over the OT limit, but it's really difficult for those of 
us who did this for a living to read posts from people who don't know 
what it takes to actually do.


On 1/17/2015 10:54 AM, KENT TRIMBLE wrote:
Otherwise known as the strategy perfected by JPL in 1998 for the Mars 
Climate Orbiter . . . one in English units and the other in metric.


K9ZTV 


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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Walter Underwood
This is getting pretty far off topic, even for someone who has been writing 
software for 30 years. See you on the 66 foot band.

A private response might be a good idea. Or hey, a sked!

wunder
K6WRU
CM87wj
http://observer.wunderwood.org/

On Jan 17, 2015, at 12:18 PM, Bill Gerth billge...@embarqmail.com wrote:

 Then, would you be so kind as to enlighten us?
 
 73,
 BILL
 W4RK
 
 On Jan 17, 2015, at 1:41 PM, Lynn W. Taylor, WB6UUT 
 k...@coldrockshotbrooms.com 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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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Merv Schweigert

Used to think it was reading comprehension,   but

K9FD/KH6


Good quips always sail over at least one person's head.

K9ZTV


On 1/17/2015 1:09 PM, Lynn W. Taylor, WB6UUT wrote:
Totally different.  This was not flight software -- and it wasn't 
all software, either.


I'm sure we're over the OT limit, but it's really difficult for those 
of us who did this for a living to read posts from people who don't 
know what it takes to actually do.


On 1/17/2015 10:54 AM, KENT TRIMBLE wrote:
Otherwise known as the strategy perfected by JPL in 1998 for the 
Mars Climate Orbiter . . . one in English units and the other in 
metric.


K9ZTV 


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Version: 2015.0.5645 / Virus Database: 4260/8946 - Release Date: 
01/17/15





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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Lynn W. Taylor, WB6UUT
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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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Phil Wheeler

I wonder if the design not being done to spec
/
//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),/


qualifies as a bug -- vs. a design mistake?

Phil W7OX

On 1/17/15 12:30 PM, KENT TRIMBLE 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 would 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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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Guy Olinger K2AV
On Sat, Jan 17, 2015 at 4:40 PM, Dick Dievendorff d...@elecraft.com wrote:

 Software work helps one with humility...


If software developing hasn't already beaten one into mumbling and slurring
of words without any assistance from the juice.

I remember so many days going home with a splitting headache, literal pain.

73, Guy.
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Re: [Elecraft] Buggy software OT

2015-01-17 Thread Fred Townsend
I think there is a big difference in flight software. In Boeing airplanes
the pilot is assisted by software. In Airbuses the pilot is allowed to fly
the airplane if the software thinks he/she is qualified. There has been at
least one airbus crash blamed on software and several other questionable
crashes. 
Unix has a dam-it key. (Dam it let me do this even though you (the computer)
think it's wrong.) I bet the airbus pilots wish they had one too.

Fred, AE6QL

-Original Message-
From: Elecraft [mailto:elecraft-boun...@mailman.qth.net] On Behalf Of ANDY
NEHAN
Sent: Saturday, January 17, 2015 12:19 AM
To: elecraft@mailman.qth.net
Subject: [Elecraft] Buggy software

Many moons ago I worked at a bank (software dept) and we had been running a
daily check reading program reading the magnetic line from a check and
sorting accordingly. Well this program read 600,000 checks a day - every
working day of the year (that's about 250) then after it had been running
about 6 years it fell over one day - a particular combinations of checks and
the way they were batched. Now that sounds to me like a LOT of testing
(600,000 * 250 * 6 = 900 million). So to expect all software to be perfect
is not realistic. As to not using or trusting software - well whatever you
do don't fly as all modern aircraft are software platforms!!
Andy G4HUE

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