uav-modeling
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Georacer
A collection of mathematical and physics equations for UAV modeling
z = r_0*h/(r_0 + h) in atmosphere model should be z = r_0*h/(r_0 - h)
Referring to the distance between center-of-mass and center-of-lift and center-of-thrust and center-of-mass.
Examine alternative wind gust models - http://www.flightsimaviation.com/data/FARS/part_25-appG.html - http://www.flightsimaviation.com/data/FARS/part_23-333.html and examine their inclusion.
Conversions between Euler angles and quaternions and quaternion propagation in the context of aerospace applications is an important aspect and should be covered.
Apparently accelerometers don't include the Corriolis acceleration in their measurements. Find out why and correct the text.