Engineering, 13.10.2020 03:01 caydennnnn5764
Starting with the three translational equations and the three moment equations for an aircraft derived. Rewrite these equations for a spin-stabilized bullet. Equations are given below:
m(U+ QW-VR)= -mgSinφ + FAx+ FPx
m(V+ RU- PW)= mg Cosφ + FAy+ FPy
m(W+ PV-QU)= mgCosφ +FAz+ FPz
a. The bullet is fired along the body y-axis, at pitch attitude angle zero degrees, and is spin stabilized.
b. Do not derive the equations from first principles.
c. Clearly state all of your assumptions.
Answers: 3
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