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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 /2219/CH11/EX11.8/Ex11_8.sce | |
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Diffstat (limited to '2219/CH11/EX11.8/Ex11_8.sce')
| -rwxr-xr-x | 2219/CH11/EX11.8/Ex11_8.sce | 14 |
1 files changed, 14 insertions, 0 deletions
diff --git a/2219/CH11/EX11.8/Ex11_8.sce b/2219/CH11/EX11.8/Ex11_8.sce new file mode 100755 index 000000000..24bfab029 --- /dev/null +++ b/2219/CH11/EX11.8/Ex11_8.sce @@ -0,0 +1,14 @@ +// Chapter 11 example 8
+//------------------------------------------------------------------------------
+clc;
+clear;
+// Given data
+Apogee = 30000; // Apogee pt of satellite elliptical orbit
+Perige = 1000; // perigee pt of satellite elliptical orbit
+
+// Calculations
+a = (Apogee + Perige)/2; // semi major axis
+
+// output
+mprintf('Semi-major axis = %d Km',a);
+//------------------------------------------------------------------------------
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