5. Consider an aircraft flying due east along the equator. Define an Earth-fixed coordinate system FE at zero longitude and zero latitude, and a local horizontal coordinate system FH fixed to the center-of-gravity (CG) of the aircraft. Describe the relationship between the axes of FE and FH at the instant the aircraft is at zero longitude and zero latitude, and again at the instant it is at 180 deg east longitude and zero latitude.

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Chapter1: Units, Trigonometry. And Vectors
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5. Consider an aircraft flying due east along the equator. Define an Earth-fixed coordinate
system FE at zero longitude and zero latitude, and a local horizontal coordinate
system F, fixed to the center-of-gravity (CG) of the aircraft. Describe the relationship
between the axes of FE and FH at the instant the aircraft is at zero longitude and
zero latitude, and again at the instant it is at 180 deg east longitude and zero latitude.
6. Assume the Earth (uniform sphere) has a diameter of 6875 NM (nautical miles, NM).
The aircraft in Problem 5 is flying at 600 knots relative to an assumed stationary
atmosphere, at a constant altitude of 2 NM. Find {@7}# and {w#}#•
EC
Transcribed Image Text:5. Consider an aircraft flying due east along the equator. Define an Earth-fixed coordinate system FE at zero longitude and zero latitude, and a local horizontal coordinate system F, fixed to the center-of-gravity (CG) of the aircraft. Describe the relationship between the axes of FE and FH at the instant the aircraft is at zero longitude and zero latitude, and again at the instant it is at 180 deg east longitude and zero latitude. 6. Assume the Earth (uniform sphere) has a diameter of 6875 NM (nautical miles, NM). The aircraft in Problem 5 is flying at 600 knots relative to an assumed stationary atmosphere, at a constant altitude of 2 NM. Find {@7}# and {w#}#• EC
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