Section B-Specify Statement as True/False 1 2 4 5 6 7 8 9 10 An aircraft does not distinguish it is the pilot who is cha

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Section B Specify Statement As True False 1 2 4 5 6 7 8 9 10 An Aircraft Does Not Distinguish It Is The Pilot Who Is Cha 1 (89.84 KiB) Viewed 18 times

Section B-Specify Statement as True/False 1 2 4 5 6 7 8 9 10 An aircraft does not distinguish it is the pilot who is changing the aero- dynamic forces on the aircraft, or it is the atmospheric turbulences which is doing so In writing aircraft equations of motion, it is not important which direc- tion aircraft is flying. Therefore, the aircraft heading angle has no role in the aircraft flying qualities Based on the Newton's 2nd law, aircraft equations of motion consist of six equations. However, when we set the magnitude of the pitch angle, they divide into two sets of longitudinal and lateral-directional equa- tions; where each set has only thee equations The relative importace of C₁ is greater than C₁₂ All longitudinal derivatives could be calculated with the same level of accuracy The relative importace of C₁ is the same as C₁ We are able to calculate all lateral-directional derivatives require +/- %10 accuracy The relative importace of C₁ is greater than ma we desire C to be positive which means we desire drag to increase once speed increases True False