Douglas DC-3( attitude_indicator.1 = 2 ) [altimeters] ขยายตาราง altimeter.0 to altimeter.n If the parameter is set to 1, a separate altimeter is instantiated, which will operate independently of other altimeters, and can have failures applied to it. Airbus A321...
The nonlinear model for the aircraft flight attitude is given by following relations (using nomenclature of Table 1): Table 1. Nomenclature V True Air Speed (TAS) α angle of attack β angle of sideslip P roll rate Q pitch rate R yaw rate ϕ bank angle θ elevation angle ψ heading...
And these entry criteria are “enforced” and protected by professional associations that are charged with protecting the individual members by protecting the criteria that limit entry into the procession or discipline and also enforce by their very existent silos of mind and attitude for the those ...
This configuration causes the aircraft 10 to sit in nose-high trim when taxiing, but allows a nearly ideal take-off attitude with little or input from the pilot. During take-off, as the aircraft 10 transitions toward takeoff speed, the aircraft 10 begins to plane on the forward portion 32...
In other words, set the airplane in the desired attitude and then use trim to hold the airplane in that attitude where your input is no longer required. 换句话说,把飞机设置在所需的姿态上,然后再用配平来保持在一个不再需要输入的姿态上。【注解:也就是说实际姿态和最初计划的理论上的理想姿态...
Basically My attitude is to fill the main centre tanks then just adjust the AUX tanks automatically to fill to the amount of excess fuel required. You can "Extend Controls" (bottom left) of the Weight and Fuel Quantities to load the different Cargo Compartments, Upper and Lower decks... ...
Aircraft trim holds control surfaces (rudder, elevator, or ailerons) in a specific position, requiring less manual input from the pilot to maintain a desired flight attitude. Trim either moves entire control surfaces (like on a stabilator) or is installed as a separate trim tab (like on an...
The new method provides a flexible way to overcome the issues of unknown flow direction at any flight attitude. Sign in to download hi-res image Fig. 44. Measured coherence length in stream-wise direction after consideration of flow angle. Comparison with model predictions. Sign in to download...
The other part is whether the internal weapons have an optimal attitude angle when the store reaches to the safe distance, which is an urgent problem for the store designers [11], [12]. In order to predict the compatibility of aircraft-store separation, it is necessary to carry out the ...
push the nose down and roll the wings level if the aircraft is in a bank. This action reduces the angle of attack and reattaches the airflow over the wing. Once recovered, the aircraft can be pulled back from the nose-down attitude and power added to get back on the previous flight ...