Method for longitudinal plane ballistic control of high altitude gliding UUV
A plane and ballistic technology, applied in the field of UUV control, can solve the problems of accurately specifying the initial state of the system, the optimal guidance method cannot modify the control instructions in real time, and the operation accuracy is reduced.
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[0043] Embodiments of the present invention are described in detail below, and the embodiments are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.
[0044] For the definition of the coordinate system relevant to the control method designed by the present invention, see figure 2 . Define the ground coordinate system {E} with its origin O E Somewhere in the horizontal plane, X E along the horizontal plane, Y E straight up. Define the body coordinate system {B} with its origin O B Located at the centroid of the UUV body, X B Pointing to the head along the UUV main axis, Y B perpendicular to X B up. Define O B The coordinates in the ground coordinate system are (x,y). Define the speed of the UUV as v. Define the pitch angle θ of the UUV as X B with X E angle, and from X BGo counterclockwise to X E is positive. Define the attack angle α of UUV as v and X B Angle of , and turn counterclockwise ...
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