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Archive for the ‘The human machine interface’ Category

Why We Automate Failure A recent post on the interface issues surrounding the use of side-stick controllers in current generation passenger aircraft led me to think more generally about the the current pre-eminence of software driven visual displays and why we persist in their use even though there may be a mismatch between what they [...]

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Airbuses side stick improves crew comfort and control, but is there a hidden cost? The Airbus FBW side stick flight control has vastly improved the comfort of aircrew flying the Airbus fleet, much as the original Airbus designers predicted (Corps, 188). But the implementation also expresses the Airbus approach to flight control laws and that [...]

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One of the less often considered aspects of situational awareness in the cockpit is the element of knowing what the ‘guy in the other seat is doing’. This is a particularly important part of cockpit error management because without a shared understanding of what someone is doing it’s supremely difficult to detect errors. The replacement of the central control stick with side stick ‘glass’ controllers eliminates a little acknowledged means of coordinating a common understanding of control inputs between aircrew with the potential for a hazardous loss of crew error management.

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Reading through the BEA’s precis of the data contained on AF447′s Flight Data Recorder you find that during the final minutes of AF447 the aircrafts stall warning ceased, even though the aircraft was still stalled. This loss of stall warning removed a significant cue to the aircrew that they had flown the aircraft into a deep stall, undoubtedly adding to their confusion. SU4CF4KDVSWQ

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One of the areas of human factors in design is the physical layout of a seated workstation or control console to suit the functional reach capabilities of the user population. Should be simple right? Wrong.

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Good and bad in the design of an Oliver Hazard Perry class frigates ECS propulsion control console HMI.

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According to the preliminary ATSB report the crew of QF32 took approximately 50 minutes to process all the Electronic Centralised Aircraft Monitor (ECAM) messages. So, two questions for the ATSB. First would the normal three man crew have been able to handle the ECAM checklist work as readily? Second should the checklist processing have taken 50 minutes which is a very, very, long time in a mid air emergency?

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Because they have typically pitch unity ratios (1:1) scales, aircraft primary flight displays provide a pitch display that is limited by the vertical field of view. This display can move very rapidly and be difficult to use in unusual attitude recoveries becoming another adverse performance shaping factor for aircrew in such a scenario. Trials by the USAF have conclusively demonstrated that an articulated style of pitch ladder can reduce disorientation of aircrew in such situations.

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Recent work in complexity and robustness theory for engineered systems has highlighted that the architecture with which these systems are designed inherently leads to ‘robust yet fragile’ behavior. This vulnerability has strong implications for the human operator when he or she is expected to intervene in response to the failure of system.

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How the design of the Apollo Command Module Attitude Reference Indicator illustrates the importance of cultural cliches or precedents in coordinating human and software behaviour.

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How even apparently simple interfaces can contain subtle error traps Back in the day learner drivers of the then new M 113 were found to be repeatedly veering off the road or into oncoming traffic when trying to carry out an emergency stop. In some circumstances learner drivers would also accelerate while trying to perform [...]

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Reflections on design errors in the human machine interface Having recently bought a new car I was driving home and noticed that the illuminated lighting controls were reflected in the right hand wing mirror. See the picture below for the effect. These sort of reflections are at best annoying, but in the worst case they could mask [...]

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The fallout from the QF 72 in flight accident has now reached the courts with Australian Aviation reporting that passengers and crew have taken up a joint class action against Airbus and Northrop Grumman (the manufacturer of the faulty Air Data Inertial Reference Unit).

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The effective use by humans of any transport system is a critical success factor in the development of such systems. Careful consideration of the interaction of ergonomic and functional design with the physical and cognitive capabilities and limitations of crew, passengers and maintainers is essential to assure safe, effective and profitable rail operations.

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The reality is that when pilots fly through an icing event or a driver steers through a skid the aircraft or car is not intelligent, the intelligence is actually in the head of the designer, the automation is merely his proxy.

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 5.3.16.3 (4)   The pedal design and/or operation shall be such that it cannot be over-ridden or tampered with in order to negate the safety feature.    State Rail Authority (SRA) specification (5.3.16.3)   On the 31st of January 2003 at approx. 7:14 am a four car Tangara passenger train on run C311 from Sydney Central to Port Kembla (G7) oversped on a downhill [...]

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