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- Path: src.honeywell.com!not-for-mail
- From: graba@htc.honeywell.com (Lee Graba)
- Newsgroups: comp.lang.ada,comp.lang.c,comp.lang.c++
- Subject: Re: C/C++ knocks the crap out of Ada
- Date: 20 Feb 1996 12:29:38 CST
- Organization: Honeywell Technology Center, Honeywell Inc.
- Message-ID: <4gd3ui$6fi@moon.src.honeywell.com>
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- In-Reply-To: <312992F6.588D@lfwc.lockheed.com>
- To: Ken Garlington <GarlingtonKE@lfwc.lockheed.com>
-
- In article <312992F6.588D@lfwc.lockheed.com>,
- Ken Garlington <GarlingtonKE@lfwc.lockheed.com> writes:
- >Jon S Anthony wrote:
- >>
- >> So, does this mean that there are _no_ confirmed cases of probes lost due
- >> software? If so, I'm impressed as software has just plain _got_ to be
- >> the weakest link in the chain. 1/2 :-)
- >
- >Actually, I would say that system requirements are the weak link in the chain,
- >although the errors often tend to occur in software these days since more
- >requirements (and particularly the harder, more volatile requirements) tend to
- >be put in software.
- >
- >Three cases near and dear to my heart:
- >
- >For years, I have heard the story about how a "bug" in the F-16 flight control
- >computer caused it to roll to an inverted position when crossing the equator. I
- >have never found anything authoritative that exactly described the circumstances
- >(if anyone has this information, let me know); but there are two points to be
- >made about this:
- >
- > 1. Until relatively recently, the F-16 flight control computer didn't have any
- > software in it. It was an analog computer.
-
- Actually, the F-16A had a hybrid flight control computer. The primary flight
- control functions were performed by an analog computer, but some flight control
- gains were scheduled with respect to flight condition by a digital computer and
- fed to the analog computer. However, setting gains should not cause the above-
- described phenomenon.
-
- If such a thing did occur, it would probably be due to the Navset, which is
- usually a separate digital computer whose responsibility is to take
- measurements and then compute positions and attitudes, and associated rates.
- A software error here might cause a problem, if say, it was telling the flight
- control computer that it was flying straight and level, and suddenly told it
- that it was really upside down. The flight control computer would then try
- to right the plane, since it doesn't know good information from bad.
-
- I have heard the above story, as well, but don't know if it is true.
-
- >
- > 2. Some people believe they heard this story in terms of the behavior of a
- > handling qualities _simulation_ of the flight control system, in which
- > the environment model only contained a part of the northern hemisphere. Someone
- > decided to see what happened when you "flew off the edge of the earth."
- >
- >The other two cases are more recent and involve pilot-induced oscillations leading
- >to an aircraft crash. In both cases, the press widely reported (in at least one
- >case, quoting a senior executive at one company) that "the software got confused."
- >However, the error in both cases was due to an interaction of the control law model,
- >which can be implemented in either hardware or software, and the pilot. (The pilot
- >will probably say the control laws were wrong; the control law people will probably
- >say that the pilot operated the system outside its' limits. Both are probably right
- >:). Nonetheless, because the behavior occured in software, that's what gets the
- >blame.
- >
- >Dr. Levison's "Safeware" defines far issue much better than I just did, BTW.
-
-