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AD2S1200YST датащи(PDF) 19 Page - Analog Devices |
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AD2S1200YST датащи(HTML) 19 Page - Analog Devices |
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19 / 25 page ![]() AD2S1200 Rev. 0 | Page 18 of 24 CIRCUIT DYNAMICS AD2S1200 LOOP RESPONSE MODEL ERROR (ACCELERATION) – θIN θOUT VELOCITY k1 × k2 1–z –1 1–bz –1 1–z –1 c1–az –1 c Sin/Cos LOOKUP Figure 11. RDC System Response Block Diagram The RDC is a mixed-signal device, which uses two A/D converters to digitize signals from the resolver and a Type II tracking loop to convert these to digital position and velocity words. The first gain stage consists of the ADC gain on the Sin/Cos inputs, and the gain of the error signal into the first integrator. The first integrator generates a signal proportional to velocity. The compensation filter contains a pole and a zero, used to provide phase margin and reduce high frequency noise gain. The second integrator is the same as the first integrator and generates the output position from the velocity signal. The Sin/Cos lookup has unity gain. Values are given below for each section: • ADC gain parameter (k1nom = 1.8/2.5) ) ( ) ( 1 V V V V k REF p IN = • Error gain parameter π × = 2 10 18 2 6 x k • Compensator zero coefficient 4096 4095 = a • Compensator pole coefficient 4096 4085 = b • Integrator gain parameter 4096000 1 = c • INT1 and INT2 transfer function 1 1 ) ( − − = z c z I • Compensation filter transfer function 1 1 1 1 ) ( − − − − = bz az z C • R2D open-loop transfer function ) ( ) ( 2 1 ) ( 2 z C z I k k z G × × × = • R2D closed-loop transfer function ) ( 1 ) ( ) ( z G z G z H + = The closed-loop magnitude and phase responses are that of a second-order low-pass filter (see Figure 12 and Figure 13). To convert G(z) into the s-plane, we perform an inverse bilinear transformation by substituting for z, where T = the sampling period (1/4.096 MHz ≈ 244 ns). s T s T z − + = 2 2 Substitution yields the open-loop transfer function G(s). ) 1 ( 2 ) 1 ( 1 ) 1 ( 2 ) 1 ( 1 4 1 ) 1 ( 2 1 ) ( 2 2 2 b b T s a a T s s T s sT b a a k k s G − + × + − + × + × + + × − − × = This transformation produces the best matching at low frequencies (f << fSAMPLE). At lower frequencies (within the closed-loop bandwidth of the AD2S1200), the transfer function can be simplified to 2 1 2 1 1 ) ( st st s K s G a + + × ≅ where: b a a k k K b b T t a a T t a − − × = − + = − + = ) 1 ( 2 1 ) 1 ( 2 ) 1 ( ) 1 ( 2 ) 1 ( 2 1 Solving for each value gives t1 = 1 µs, t2 = 90 µs, and Ka ≈ 7.4 × 106 s -2. Note that the closed-loop response is described as ) ( 1 ) ( ) ( s G s G s H + = By converting to the s-domain, we are able to quantify the open-loop dc gain (Ka). This value is useful during calculation of acceleration error of the loop as discussed in the Sources of Error section. The step response to a 10° input step is shown in Figure 14. Because the error calculation (Equation 3) is nonlinear for large values of θ − ϕ, the response time for larger step changes in position (90°–180°) will typically take three times as long as the response to a small step change in position (<20°). In response to a step change in velocity, the AD2S1200 will exhibit the same response characteristics as for a step change in position. |
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