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![Airborne radar. Airplanes; Guided missiles. 2-25] ANALYSIS OF THE VECTORING PHASE 'Space Reference 109. for Error Signal Fig. 2-31 Vectoring Error Geometry. A^i = ARa/R ARa « R (2-41) where ARa =](https://c8.alamy.com/comp/RPWYTF/airborne-radar-airplanes-guided-missiles-2-25-analysis-of-the-vectoring-phase-space-reference-109-for-error-signal-fig-2-31-vectoring-error-geometry-ai-=-arar-ara-r-2-41-where-ara-=-component-of-the-relative-position-error-between-target-and-interceptor-which-is-normal-to-the-sight-line-the-vectoring-system-computes-a-desired-interceptor-lead-angle-lc-with-respect-to-the-erroneous-sight-line-angle-from-fig-2-31-the-computed-lead-angle-is-dd-dln-dd-dlp-dvr-sin-ld-=-vtf-sin-6-then-lf-cos-ld-l-lts-ld-axpt-fp-cos-ld-2-42-2-4-aft-2-43-please-note-that-th-RPWYTF.jpg "Airborne radar. Airplanes; Guided missiles. 2-25] ANALYSIS OF THE VECTORING PHASE 'Space Reference 109. for Error Signal Fig. 2-31 Vectoring Error Geometry. A^i = ARa/R ARa « R (2-41) where ARa =")
Airborne radar. Airplanes; Guided missiles. 2-25] ANALYSIS OF THE VECTORING PHASE 'Space Reference 109. for Error Signal Fig. 2-31 Vectoring Error Geometry. A^i = ARa/R ARa « R (2-41) where ARa =
