. Airborne radar. Airplanes; Guided missiles. 506 AUTOMATIC TRACKING CIRCUITS approximations to the input time function may be avoided. We pi by taking derivatives of Equation 9-7. Thus Ro (0 [-(;)']"? )ceed (9-8) "• h(0' Plots of Equations 9-7, 9-8, and 9-9 are shown in Fig. 9-19. A segment broken-line approximation of range rate is shown in Fig. (9-9) three- Fig. 9-19 Normalized Position, Velocity, and Acceleration Components of Motion for Pass-Course Range Tracking. Slope = - -At -3t -2r -f /q '^ 2t 3r 4t '0 +^ \r-0 Fig. 9-20 Approximations for Components of Motion Leading
. Airborne radar. Airplanes; Guided missiles. 506 AUTOMATIC TRACKING CIRCUITS approximations to the input time function may be avoided. We pi by taking derivatives of Equation 9-7. Thus Ro (0 [-(;)']"? )ceed (9-8) "• h(0' Plots of Equations 9-7, 9-8, and 9-9 are shown in Fig. 9-19. A segment broken-line approximation of range rate is shown in Fig. (9-9) three- Fig. 9-19 Normalized Position, Velocity, and Acceleration Components of Motion for Pass-Course Range Tracking. Slope = - -At -3t -2r -f /q '^ 2t 3r 4t '0 +^ \r-0 Fig. 9-20 Approximations for Components of Motion Leading to Please note that these images are extracted from scanned page images that may have been digitally enhanced for readability - coloration and appearance of these illustrations may not perfectly resemble the original Povejsil, Donald J. Princeton, N. J. , Van Nostrand
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Keywords: ., bookcentury1900, bookcollectionbiodiversit, booksubjectairplanes
