Step- by- step Guidete tu Calculating Satellite Antenna Gain andCoverage Area
Satellite communication relies on precise calculations to determinate antenna gain and coverage area. Zrozumiałe, że koncepty te pomagają in designing effective satellite links and ensuring optimal signal contricth. This guidede provides a step-by-step process to perfom these callations crisately.
Understanding Antenna Gain
Antenna gain measures how well an antenta directs radio frequency energy in a specific direction. It is usually expressed in decibels (dBi). Higher gain indicates a more focused beam, which can precles signal emphth and reduce interference.
Tu calculate antenna gain, you need the antenna 's physional dimensions ande thee operating frequency. The formula i s:
(dBi) = 10 * log (vd) = 10; FLT (vd): 1; FLT (vd): 1; FLT (vd): 1; Flt (vd): 1; Flt (vd): 1; Flt (vd): 1; Flt (vd): 1; Flt (vd): 1; Fl (vd): 1; Fl (vd): 1; Fl (vd); FLT (vd): 1; Flt (vd): 1; Flt (vd); Fl (vd); Fl (vd): 1; Fl (vd); Fl): 1; FLT (vd: 1; Fl); Fl: 1; Fl: 1; Fl: 1; Fl; Fl: 1; Fl; Fl: 1; Fl: 1; Fl: 1; Fl: 1; Fl: 1; Fl: 1; Fl: 1; Fl; Fl; Fl; Fl; Fl
gdy G is thee antenna 's directivity, cocalcated as:
(4 * ∞ * A) / λ λ λ (1); FLT (1); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); FLT (3); Flight (3); Flight (3); Flight (3); Flight (3); Flight (3); Flight (3); Flight (1 (3); Flight (1); Flight (1); Flight (1); Flight (1 (1); FLT (1); FLT (1); FLT (1); FLT (4): (4)
Here, A is the antenna 's effective apertura, andd λ is the fonegth of the signal.
Calculating Coverage Area
Te przykrywki są o a satellite antenna zależy od nich, że beamwidth i te te distance to o thee target area. The main parameter is thee antenna 's beamwidth, which indicates the e angular width of thee main lobe.
Te przybliżone coverage radius (R) on Earth 's surface can be calculated using:
(+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 3; (+) 1; (+) 3; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1; (+) 1) 1; (+) 1; (+) 1) 1; (+) 1) (+ (+) (+) (+) (+) (+) (+) (+) (+) (+) (+) (+))))))) 1)) 1) 1) ((((0) (+ (+ (+) (((+) ((0) (0) (0) (0) (0) (0) (0) (0) (0) (0) (0) (0) (0) (
Kiedy jest to satellite 's altequidde, i d θ is the beamwidth in degrees. The coverage area (A) is then:
(A = ∞ * R) 1; (FLT: 1); (FLT: (XI1; FLT:) 1; (XI1; FLT: 0 XI3; (FLT: 0 XI3; (XI3; A = ∞ * R XI1; (XI1; FLT: 1 XI3;) (FLT:); (XI3; 2 XI1; FLT: 2 XI3; (XI3; FLT: 3 XI3;)); (XIXI1; FLT: 3 XI3; (XIXIX3;)))
Praktyka Badanie
Pomocnik satellite operates at a frequency of 12 GHz, with an antenna diameter of 1 meter, orbiting at 35,786 km altequetde. To find the gain, first calculate the flonegth:
Xi1; Xi1; FLT: 0 X3; Xi3; λ = c / f = 3 x 10 Xi1; Xi1; FLT: 1 XI3; XI3; XI3; XI1; FLT: 2 XI3; XI3; / 12 x 10 XI1; XI1; FLT: 3 XI3; XI3; 9 XI1; FLT: 4 XI3; XI3; XI3; = 0.025 Metrów XI1; XI1; FLT: 5 XI3; XI3; FLT: 5; XIXI3; XIXI3;
Next, determinate the directivity G:
(RR): (RR: 3H; FLT: 3H; FLT: 3H; FLT: 3H; FLT: 3H; FLT: 3H; 2; FLT: 2; FLT: 3H; 3H;) / 4 = (RR * 1; FLT: 3; FLT: 3H; 2; FLT: 3H; FLT: 4; FLT: 3; FLT: 3H; FLT: 7; FLT: 3H; FLT: 3H; FLT: 3H; FLT: 6; 3H; FLT: 3H; FLT: 7; FLT: 3H; FLS; 3H; FLT; FLT: 3H; FLS; 3H; FLS; 3H; FLS; FLT: 3H; FLS; 1; FLT: 3H; FLS: 3H; FLS: 3H; FLS: 3H; FLS: 3H; FLS: 3H; F@@
Then, G = (4 * ∞ * 0.785) / (0.025) Xi1; FLT: 0 Xi3; Xi3; 2 Xi1; Xi1; FLT: 1 Xi3; Xi3; Xi3; XiX1257.2
Gain in dBi:
(1257.2) 31,99 dBi V1; (1257,2) 31,1; FLT: 3,3; FLT: 33,3; FLT: 33,3; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FLT: 3,8; FL3; FLT: 1,2,8 dBi;
For coverage, assuming a beamwidth of 2 degrees:
R = 35786 km * tan (1 °)
Coverage area:
A = ∞ * (624 km) giganty1; giganty1; FLT: 0 giganty3; giganty3; 2 giganty1; GGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGGG@@