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| author | priyanka | 2015-06-24 15:03:17 +0530 |
|---|---|---|
| committer | priyanka | 2015-06-24 15:03:17 +0530 |
| commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
| tree | ab291cffc65280e58ac82470ba63fbcca7805165 /2282/CH6/EX6.4 | |
| download | Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.gz Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.bz2 Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.zip | |
initial commit / add all books
Diffstat (limited to '2282/CH6/EX6.4')
| -rwxr-xr-x | 2282/CH6/EX6.4/ex6_4.sce | 20 |
1 files changed, 20 insertions, 0 deletions
diff --git a/2282/CH6/EX6.4/ex6_4.sce b/2282/CH6/EX6.4/ex6_4.sce new file mode 100755 index 000000000..488c35d86 --- /dev/null +++ b/2282/CH6/EX6.4/ex6_4.sce @@ -0,0 +1,20 @@ +// Example 6.4, page no-231
+clear
+clc
+
+R=42150 //orbital radius of satellite
+oi=0.25/100 // orbit inclination
+acc=0.3 //error of 0.3 degree
+c=3*10^8 // speed of light
+x=oi*R
+x=ceil(x*10)/10
+y=R*2*%pi*acc/360
+y=ceil(y*10)/10
+z=sqrt(x^2+y^2)
+z=ceil(z*10)/10
+delay=z*10^6/c
+delay=floor(delay*1000)/1000
+pd=2*delay
+printf("variation in alitude caused byorbit inclination = %.1fkm\n variation due to station-keeping error of 0.3° = %.1fkm",x,y)
+printf("\n Both these errors will introduce a maximum range variation of %.1fkm\n This cause a one-way propagation delay of %.3fms\n Round trip propagation delay =%.2fms\n Dopler Shift = %.2f ms in 8h=56.25 ns/s",z,delay,delay*2,pd)
+
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