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They also give good feedback about where the player s edge of competence is and how it is developing, as does Sonic Adventure 2 Battle Rise of Nations allows the player to customize many aspects of the difficulty level and gain feedback of whether things are getting too easy or too hard for the player Education: School is often too easy for some kids and too hard for others even when both are in the same classroom Motivation for humans lies in challenges that feel challenging but doable and in gaining continual feedback that lets them know what progress they are making Learners should be able to adjust the difficulty level while being encouraged to stay at the outer edge of, but inside, their level of competence They should gain insight into where this level is and how it is changing over time.

Good games don t come in grade levels that players must be at They realize that it doesn t matter when the player finishes or how he or she did in comparison to others all that matters is that the player learns to play the game and comes to master it Players who take longer and struggle longer at the beginning are sometimes the ones who, in the end, master the final boss most easily There are no special learners when it comes to videogames Even an old guy like me can wander the plains of Morrowind long enough to pick up the ropes and master the game.

Other de nitions such as FAR 25 are based on the cloud liquid water content and droplet size and are used in the design and testing process. For the ground icing hazard de-icing uids are universally used to ensure the aircraft surface is free of ice at take-off. The method of countering the airborne icing hazard varies depending on the nature of the aircraft and its operational requirements. These can be divided broadly into two categories, those aircraft requiring ice protection and those not. The former category contains aircraft which are clearly prohibited from ying in icing conditions and fast jet military aircraft which have the operational exibility to avoid such conditions, either by achieving an ice free speed , i.e. accelerating to a speed where surface temperatures are too high for icing to occur, or by ying around them. In this case a limited duration clearance (typically ve minutes) may be given for takeoff and landing through icing conditions by analysis of the accretion characteristics of the airframe utilising specialised icing prediction computer programs, and testing in natural icing conditions or behind icing tankers. In these cases the aircraft are often tted with ice detectors to inform pilots of the presence of icing conditions and the need to take action. Where some form of ice protection is required there are various methods utilised. A distinction is made between an anti-ice system where ice accretion is prevented, and a de-ice system where a limited amount of accretion is allowed before some action is taken to shed it. These systems are used in conjunction with an ice detector.

The world doesn t go away, I can enter any time; it gives me constant feedback, but never a final judgment that I am a failure; and the final exam the final boss is willing to wait until I am good enough to beat him..

Anti-ice systems can utilise: Hot bleed air where either continuously or when icing conditions are present, hot air is projected on the inside of a surface subject to ice accretion such as a wing leading edge or engine bullet Electrical heating where elements are embedded in the structure susceptible to icing to achieve a continuous surface temperature above freezing level Liquid ice protection where a freezing point depressant liquid is deposited on a surface or extruded through a porous surface to prevent freezing De-ice systems can utilise: Pneumatic boots where a reinforced synthetic rubber layer is overlaid on the susceptible surface and periodically in ated in conditions of ice accretion thereby breaking and shedding the ice Electrical heating which can be used in a de-icing mode by switching on and off periodically during exposure to icing conditions Electro-expulsive system which utilises opposing magnetic elds or eddy currents induced by conductors embedded in a exible surface to create relative movement and hence the breakage and shedding of the accreted ice Electro magnetic impulse de-icing which utilises coils inside the leading edge inducing eddy currents in metal skin with the result that the surface is deformed, breaking the ice All of the above have their relative advantages and disadvantages the balance of which is dependent on the operational requirements and characteristics of the target aircraft. Extensive use is made of sophisticated computer icing prediction models to determine areas requiring protection and the requirements for the protection, followed by testing of sample areas in wind tunnels and icing tunnels, and ight testing in icing conditions. Flight testing with simulated icing shapes attached to vulnerable areas of the airframe is also performed to determine handling characteristics with ice accreted.