| 摘要 |
702,654. Radio navigation. STANDARD TELEPHONES & CABLES, Ltd. Sept. 2, 1952, No. 22036/52. Class 40 (7) A radio navigation system defining an approximately spiral guide course (denoted by the thick line in the Figure) to the entrance gate 25 of an airport approach zone having a landing axis 22 comprises two responders A and B spaced transversely a distance d on either side of the axis 22. The aircraft P radiates recurrent timing signals, e.g. pulse or C.W. which are re-radiated by responder A and received by the aircraft and by responder B which further re-radiates them back to the aircraft which is provided with means for measuring and displaying the time displacements #1, #2 and #3 between (1) transmission of the signal from P and reception of the signal from B, (2) transmission from P and reception from A and (3) reception of the signals from A and B so that #1, #2 and #3 correspond to transmission paths (PA+AB+PB), 2 PA and path difference (PB+AB)#PA respectively, the lines of constant #1, #2 and #3 being respectively families of confocal ellipsis (foci A and B), concentric circles (centre A), and confocal hyperlolae (foci A and B). The desired spiral path from point 36 onwards comprises portions of ellipse 27, circle 30 and hyperbolae 33 which are tangential at points 37, 39 these curves being defined by #1 # bd, #2 = #3 # 2d or #1 = 270‹, #2 = #3 = 90‹ if C.W. tuning signals of wavelength 8d are employed. In operation the pilot first observes the 1# phasemeter and when the indicated value is 270‹ he controls the aircraft to maintain this value thereby following ellipse 27 until #2 decreases to 90‹ at point 37, #2 being then maintained constant along circle 31 until #3 decreases to 90‹ at point 39 and #3 being then maintained constant along the approach axis. Elliptical paths at different heights may be used as holding patterns for waiting aircraft. For an approach gate of width 6 km, d may be 9 km, corresponding to a 4167 c/s timing signal, the signal being transmitted from P, A and B on different carrier frequencies, Fig. 1 (not shown) and responders A and B comprising simple frequency changers, Fig. 3 (not shown). For such values ambiguities will exist but the separation between ambiguous courses is sufficient to avoid confusion. The phase meters may comprise phase discriminators operating left-right indicating meters displaying a phase range of Œ 10‹ corresponding to zones bounded by the dotted lines. |
