diff options
Diffstat (limited to 'Satellite_Communication/chapter_2.ipynb')
| -rw-r--r-- | Satellite_Communication/chapter_2.ipynb | 18 |
1 files changed, 0 insertions, 18 deletions
diff --git a/Satellite_Communication/chapter_2.ipynb b/Satellite_Communication/chapter_2.ipynb index 233fcb29..62e9c6de 100644 --- a/Satellite_Communication/chapter_2.ipynb +++ b/Satellite_Communication/chapter_2.ipynb @@ -27,7 +27,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''satellite velocity'''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -68,7 +67,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''orbit parameters'''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -122,7 +120,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbit parameters'''\n",
"#Variable Declaration\n",
"ma=42000.0 # Major axis distance in Km\n",
"P=8000.0 # Perigee distance in Km\n",
@@ -161,7 +158,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbit parameters'''\n",
"\n",
"#Variable Declaration\n",
"e=0.6 #Eccentricity\n",
@@ -204,7 +200,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbit Eccentricity'''\n",
"#Variable Declaration\n",
"AP_diff=30000.0 #difference between apogee and perigee in km\n",
"AP_sum=62800.0 #Apogee+perigee\n",
@@ -242,7 +237,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Velocity of satellite at particular point '''\n",
"import math\n",
"#Variable Declaration\n",
"R=7000.0*10**3 # sattelite orbit in m\n",
@@ -287,7 +281,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Velocity of satellite at particular point '''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -330,7 +323,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Velocity of satellite at particular point '''\n",
"import math\n",
"#Variable Declaration\n",
"R=25000.0*10**3 #sattelite orbit in m\n",
@@ -373,7 +365,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbital time period'''\n",
"import math\n",
"#Variable Declaration\n",
"a=(50000.0/2)*10**3 #Semi-major axis in m\n",
@@ -417,7 +408,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbital time period'''\n",
"#Variable Declaration\n",
"a1=18000.0*10**3 #Semi-major axis for first satellite in m\n",
"a2=24000.0*10**3 #Semi-major axis f0r 2nd satellite in m\n",
@@ -453,7 +443,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbit parameters'''\n",
"import math\n",
"#Variable Declaration\n",
"a=25000.0*10**3 #appogee distance in m\n",
@@ -533,7 +522,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Velocity at apogee'''\n",
"#Variable Declaration\n",
"A=42000.0 # Apogee in km\n",
"P=8000.0 # Perigee in km\n",
@@ -572,7 +560,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''velocity of satellite at particular point'''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -614,7 +601,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''New apogee distance'''\n",
"import math\n",
"#Variable Declaration\n",
"A1=12000.0 # first Apogee distance\n",
@@ -658,7 +644,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''satellite velocity'''\n",
"import math\n",
"#Variable Declaration\n",
"vp=8.0 # horizontal velocity of satellite in km/s\n",
@@ -700,7 +685,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Apogee distance'''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -750,7 +734,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Height of satellite orbit above eart surface'''\n",
"\n",
"import math\n",
"#variable declaration\n",
@@ -792,7 +775,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Orbital time period'''\n",
"import math\n",
"#variable declaration\n",
"\n",
|