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It is simply the rate at which the aircraft can pitch - ie. rotate around the lateral axis, which is roughly the wings. The faster an aircraft can pitch, the greater the "g" limit required, and achieved. Otherwise it would become overstressed. Most aircraft can exceed their 'G' Limits, but pilots prevent this through "seat of the pants" indications of wing loading.
What else can I help you with?
What is roll rate in reference to aircraft?
Roll, pitch, and yaw - flight dynamics. See the below link for more info.
What is an aircraft blade paddle?
It is a tool used to manualy change the pitch of an variable pitch aircraft propeller.
What is the aircraft crash rate on an aircraft carrier?
The crash rate of aircraft landing on an aircraft carrier is 2.15 for every 100,000 touchdowns. The arrestor hook malfunctions or does not catch a cable on approximately 10% of landings.
What is meant by longitudinal dynamics of aircraft?
Longitudinal aircraft dynamics variables are (small) deviations from operating point or trim conditions state (components): u: velocity of aircraft along body axis v: velocity of aircraft perpendicular to body axis (down is positive) : angle between body axis and horizontal (up is positive) q : angular velocity of aircraft (pitch rate)
What control surface controls pitch?
The control surface that controls pitch is the elevator. It is located on the horizontal stabilizer of an aircraft and is used to control the aircraft's pitch attitude by adjusting the angle of the stabilizer.
What is used to control pitch of an aircraft?
elevator
What does the elevator do for an airplane?
controls aircraft pitch
What is pitch in aircraft?
Pitch is a rotating movement of the body of the aircraft about the axis of the wings. Pitch is represented by rotating to tilt the aircraft up or down. Yaw is a rotation left and right, similar to turning your head to the left and right. Roll is a rotation of the aircraft about the front to rear axis. An aircraft would roll if the pilot wanted to turn it to fly upside down.
What does pitch control in an airplane?
Pitch controls the angle up or down of the aircraft.
Does the rudder control the pitch?
No, the rudder does not control the pitch of an aircraft. The rudder is primarily used for controlling yaw, which is the side-to-side movement of the aircraft's nose. Pitch is controlled by the elevator, which is located on the tail of the aircraft and adjusts the angle of the plane's nose up or down.
What is the pitch of an aircraft?
The pitch of the aircraft is the amount of rotation along the lateral axis. The lateral axis runs along the wingspan, therefore the pitch is the amount that the nose of the plane is above or below that axis.
How does a aeroplane move?
Elevators control the pitch (up and down) of the aircraft. Ailerons control the roll of the aircraft. And rudders control the yaw of the aircraft.
