Image from page 529 of "Airborne radar" (1961)
Title: Airborne radar
Identifier: airborneradar00pove
Authors: Povejsil, Donald J
Subjects: Airplanes; Guided missiles
Publisher: Princeton, N. J. , Van Nostrand
Contributing Library: MBLWHOI Library
Digitizing Sponsor: Boston Library Consortium Member Libraries
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Text Appearing Before Image:
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- 9-20a.
Text Appearing After Image:
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 Impulses.
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