Last sentence should be changed to read: "Other pseudo forces and moments can result from gyroscopic effects of objects attached to the vehicle such as propellers and turbine blades, or forces and moments resulting from the rotation of the aircraft relative to an inertial coordinate frame."
Spurious exclamation mark should be removed after the word "rate".
The phrase that reads: "Because mass is a scalar, Eq. (5.1.1) can be rearranged as" should be changed to read: "All vectors in this equation are expressed in body-fixed coordinates. Rearranging gives"
The phrase that reads: "often referred to as the Coriolis acceleration." should be changed to read: "a rotational transport term that results from expressing the velocity vector in the rotating body-fixed coordinate system. It is sometimes referred to in the flight-dynamics literature as a Coriolis coupling term [69]."
The phrase that reads: "what is called the Coriolis force." should be changed to read: "a corresponding force."
Step 5 in the pseudo code should read "Eqs. (C.1.5)-(C.1.10)
Step 6 should be deleted
The first sentence should be changed to read: "In a steady coordinated turn, the side force due to gravity and bank angle perfectly balance the side force produced by the rotational transport terms in Eq. (6.1.9)."
The phrase that reads: "the third component is the dimensionless Coriolis acceleration." should be changed to read: "the third component includes the dimensionless rotational transport terms discussed in Section 5."
The phrase that reads: "Coriolis accelerations." should be changed to read: "rotational transport terms discussed in Section 5.1."