Sine-cosine function IP core capable of reconfiguring spaceborne computer and control method thereof

The invention relates to a sine-cosine function IP core capable of reconfiguring a spaceborne computer and a control method thereof, relating to the technical field of aerospace electronics, and solving the problems that the result of initial value assignment is largely influenced due to rounding errors, and the larger the angle is, the more the iteration times is needed. An initializing module is connected with a right-shift N-bit module and a module 1, the module 1 is connected with a cosine value storing device, the right-shift N-bit module is connected with a sine value storing device, the cosine value storing device and the sine value storing device are connected with a subtracter-adder and a first multiplier, the subtracter-adder is connected with a second multiplier and then is connected with the cosine value storing device, the first multiplier is connected with a left-shift 1-bit module and then is connected with the sine value storing device, and the a controller is connected with the sine value storing device and the cosine value storing device. The control method comprises the following steps of: mapping eta into [0, pi/2] to generate theta; judging whether theta is less than and equal to beta; if theta is less than and equal to beta, directly assigning the value and carrying out the last step; otherwise, carrying out the iteration operation, and obtaining an assigned initial value according to an approximate rule; calculating by utilizing a double-angle formula, judging whether n is less than N; if n is less than N, calculating again; otherwise, finishing the operation; finally assigning a sine/cosine function value according to the positive/negative result obtained by the sign bit judgment. The invention is applied to attitude control.