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The bounded stability of the system is proved, and the results are illustrated through a simulation example where the airship is submitted to a large airspeed variation.
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As power output is proportional to the cubic power of the incident airspeed, any small increase in the incident wind yields a large increase in the energy output.
Since all our data were collected at a ground speed of 70 mph (113 km/h), Figure 3 shows that there can be a large variation of fuel economy for the same ground speed,simply because the airspeed can be very different.
The input power to the hot wire is then a measure of airspeed, and a meter in the electrical circuit of the hot wire can be calibrated to indicate airspeed.
Open image in new window Figure 1 Fuel economy as a function of airspeed for a 2003 Chevy Suburban.
The results of this investigation show that our theoretical model correctly describes the experimental data on fuel economy of a vehicle as a function of airspeed.
In small private aircraft, the instrumentation is simple and may consist only of an altimeter to register height, an airspeed indicator, and a compass.
There's a number of reasons why an airspeed sensor could malfunction, including a build-up of ice.
A traditional mechanical airspeed indicator contains a pressure diaphragm that is connected to the pitot tube.
An autogiro had to taxi for takeoff, and it required a forward airspeed in order to drive its rotor.
On a quadcopter, airspeed isn't all that important, but it definitely matters when you want to keep a plane in the air.
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