1 00:00:03,772 --> 00:00:05,980 We would now like to calculate the potential function 2 00:00:05,980 --> 00:00:08,890 for a universal law of gravity. 3 00:00:08,890 --> 00:00:11,382 So let's set up a coordinate system first. 4 00:00:11,382 --> 00:00:13,840 And in this case, we're going to make a very special case-- 5 00:00:13,840 --> 00:00:17,200 although, the general result doesn't depend on that. 6 00:00:17,200 --> 00:00:21,130 So suppose we have a planet of radius rp 7 00:00:21,130 --> 00:00:23,410 and we have a small object. 8 00:00:23,410 --> 00:00:25,840 And initially, our object is a distance r 9 00:00:25,840 --> 00:00:27,130 away from the planet. 10 00:00:27,130 --> 00:00:30,070 This is our initial state. 11 00:00:30,070 --> 00:00:32,290 And the planet has mass to the planet. 12 00:00:32,290 --> 00:00:34,380 And our small object has m. 13 00:00:34,380 --> 00:00:35,980 And this object is moving. 14 00:00:35,980 --> 00:00:38,320 Of course, orbits really aren't like that, 15 00:00:38,320 --> 00:00:40,870 so we should be a little bit more careful. 16 00:00:40,870 --> 00:00:46,780 But our orbit might be some type of hyperbolic section-- conic 17 00:00:46,780 --> 00:00:47,950 section. 18 00:00:47,950 --> 00:00:53,830 And the orbit over here is at some final position. 19 00:00:53,830 --> 00:00:57,790 In our eyes, the distance from the object to the center 20 00:00:57,790 --> 00:01:00,750 of the planet as our final is. 21 00:01:00,750 --> 00:01:04,390 Now because there's a central point to this problem, 22 00:01:04,390 --> 00:01:06,790 the natural coordinate system to use 23 00:01:06,790 --> 00:01:10,360 is polar coordinates in the plane. 24 00:01:10,360 --> 00:01:15,100 And let's just imagine that at this moment 25 00:01:15,100 --> 00:01:17,890 we have the universal force of gravity. 26 00:01:17,890 --> 00:01:19,300 Here's our object. 27 00:01:19,300 --> 00:01:22,630 And it's being displaced a distance s. 28 00:01:22,630 --> 00:01:28,420 So our coordinate system is polar. 29 00:01:28,420 --> 00:01:33,970 Let's call r hat this way and theta hat that way. 30 00:01:33,970 --> 00:01:36,490 And let's blow up our little displacement 31 00:01:36,490 --> 00:01:38,259 in terms of our coordinate system, 32 00:01:38,259 --> 00:01:40,910 just so that we see what's happening. 33 00:01:40,910 --> 00:01:50,500 So let's imagine that our little ds 34 00:01:50,500 --> 00:01:54,310 vector is pointing like this. 35 00:01:54,310 --> 00:01:58,900 And our center point here, we have tge r hat pointing 36 00:01:58,900 --> 00:02:02,740 radially outward and the theta hat 37 00:02:02,740 --> 00:02:04,470 pointing towards the center. 38 00:02:04,470 --> 00:02:08,620 Now to exaggerate this picture, if this is r, 39 00:02:08,620 --> 00:02:13,030 then the arc length here is rd theta. 40 00:02:13,030 --> 00:02:18,610 And the difference as the object moves from one 41 00:02:18,610 --> 00:02:27,142 point here to a closer point towards the center, will be dr. 42 00:02:27,142 --> 00:02:32,530 And so our ds vector, we can write as a radial piece r hat. 43 00:02:32,530 --> 00:02:34,390 Now, I don't put a sign in there, 44 00:02:34,390 --> 00:02:36,160 because only the end points of my integral 45 00:02:36,160 --> 00:02:38,290 will tell me whether I was going towards the planet 46 00:02:38,290 --> 00:02:39,660 or away from the planet. 47 00:02:39,660 --> 00:02:42,670 And rd theta, theta hat. 48 00:02:42,670 --> 00:02:45,370 And our gravitational force is minus 49 00:02:45,370 --> 00:02:50,960 g mass mass of the planet over the distance squared r hat. 50 00:02:50,960 --> 00:02:53,440 So now what we see is that when we 51 00:02:53,440 --> 00:02:56,890 take the dot product of these two forces, 52 00:02:56,890 --> 00:02:59,920 r hat dot r hat is 1 in polar coordinates. 53 00:02:59,920 --> 00:03:03,490 Why is that the case, r hat dot r hat is 1? 54 00:03:03,490 --> 00:03:06,970 Because these vectors are in the same direction, 55 00:03:06,970 --> 00:03:08,830 the angle between them is 0. 56 00:03:08,830 --> 00:03:12,550 And remember, that any two vectors that are perpendicular 57 00:03:12,550 --> 00:03:14,320 have dot product 0. 58 00:03:14,320 --> 00:03:17,320 r hat and theta hat are perpendicular. 59 00:03:17,320 --> 00:03:19,550 And so r hat dot r hat is 1. 60 00:03:19,550 --> 00:03:21,420 r hat dot theta hat is 0. 61 00:03:21,420 --> 00:03:29,500 And so we only get minus GMP r squared dr. 62 00:03:29,500 --> 00:03:32,740 And that's the first step in calculating 63 00:03:32,740 --> 00:03:39,310 our potential difference because U of r final minus U of r 64 00:03:39,310 --> 00:03:43,840 initial by definition is minus the work done in going 65 00:03:43,840 --> 00:03:46,990 from the initial state to the final state, which 66 00:03:46,990 --> 00:03:48,910 are described by these parameters r initial 67 00:03:48,910 --> 00:03:54,130 and r final of F gravitation dot ds. 68 00:03:54,130 --> 00:03:58,120 And now we have, actually, minus sign 69 00:03:58,120 --> 00:04:03,040 in the definition, another minus sign coming from the dot 70 00:04:03,040 --> 00:04:04,450 product. 71 00:04:04,450 --> 00:04:06,550 And lets make this our integration variable, 72 00:04:06,550 --> 00:04:11,489 r prime, r initial, r prime equals r final. 73 00:04:11,489 --> 00:04:13,030 And there's going to be a third minus 74 00:04:13,030 --> 00:04:17,680 sign because the integral of dr r prime squared is minus 1 75 00:04:17,680 --> 00:04:20,110 over r prime. 76 00:04:20,110 --> 00:04:22,210 So there would be 3 minus signs-- one 77 00:04:22,210 --> 00:04:25,150 from the definition, one from the scalar product, 78 00:04:25,150 --> 00:04:26,860 and one from the integration. 79 00:04:26,860 --> 00:04:32,560 And so we get r final minus r initial equals 3 minus signs 80 00:04:32,560 --> 00:04:36,770 given overall minus sign planet and planet 81 00:04:36,770 --> 00:04:41,770 1 over r final minus 1 over r initial. 82 00:04:41,770 --> 00:04:45,460 So this is the change in gravitational potential energy 83 00:04:45,460 --> 00:04:48,760 as my small object goes from some initial state 84 00:04:48,760 --> 00:04:51,770 to some final state. 85 00:04:51,770 --> 00:04:53,350 What about the potential function? 86 00:04:53,350 --> 00:04:56,590 Where should we choose our reference point? 87 00:04:56,590 --> 00:05:01,750 So our reference state here is a little bit unusual. 88 00:05:01,750 --> 00:05:05,590 And it will be at infinity. 89 00:05:05,590 --> 00:05:09,820 And we'll choose as a potential for our reference potential 90 00:05:09,820 --> 00:05:14,050 to be 0 at infinity. 91 00:05:14,050 --> 00:05:16,840 Imagine initial state very, very far away from the planet. 92 00:05:19,630 --> 00:05:25,570 And we'll take us a final state, an arbitrary state, 93 00:05:25,570 --> 00:05:29,560 just where the object is some distance r from the planet. 94 00:05:29,560 --> 00:05:31,990 Now, we have to be a little bit careful, 95 00:05:31,990 --> 00:05:36,159 because in this calculation our final state must always 96 00:05:36,159 --> 00:05:38,420 be outside the planet. 97 00:05:38,420 --> 00:05:39,940 And the reasons for that is subtle, 98 00:05:39,940 --> 00:05:42,400 but the gravitational force inside the planet 99 00:05:42,400 --> 00:05:46,600 is no longer minus g and 1 M2 over r-squared. 100 00:05:46,600 --> 00:05:51,890 So our analysis only applies for r bigger than r planet. 101 00:05:51,890 --> 00:05:55,930 And if we put these values for r and infinity in here, 102 00:05:55,930 --> 00:06:00,160 we get U of r minus the potential at our reference 103 00:06:00,160 --> 00:06:05,110 point, which will be 0, equals minus GMNP. 104 00:06:05,110 --> 00:06:07,240 And here's the reason why we choose 105 00:06:07,240 --> 00:06:12,460 that reference point, 1 over r arbitrary state is just minus 1 106 00:06:12,460 --> 00:06:13,300 over r. 107 00:06:13,300 --> 00:06:17,950 But 1 over infinity, if we use the initial state 108 00:06:17,950 --> 00:06:20,500 as the reference point, 1 over infinity is 0. 109 00:06:20,500 --> 00:06:23,470 So that's minus 0. 110 00:06:23,470 --> 00:06:27,550 And so what we get is that the potential function 111 00:06:27,550 --> 00:06:31,090 is equal to our reference potential-- 112 00:06:31,090 --> 00:06:37,780 actually, minus GM mass of the planet over r for r 113 00:06:37,780 --> 00:06:41,380 bigger than our reference. 114 00:06:41,380 --> 00:06:43,990 And that is the potential function 115 00:06:43,990 --> 00:06:46,760 for the gravitational problem. 116 00:06:46,760 --> 00:06:51,409 But now remember, we're choosing that to be our reference point. 117 00:06:51,409 --> 00:06:56,950 And so the real conclusion is U of r equals minus GMN 118 00:06:56,950 --> 00:07:02,020 planet over r with U at infinity equals to 0. 119 00:07:05,880 --> 00:07:08,820 Now, let's just finish this by saying in words 120 00:07:08,820 --> 00:07:11,770 precisely what this means. 121 00:07:11,770 --> 00:07:15,030 So if I start my system at infinity 122 00:07:15,030 --> 00:07:19,110 and I end my system a distance r away from the planet, 123 00:07:19,110 --> 00:07:23,010 and I calculate the work done by the gravitational force 124 00:07:23,010 --> 00:07:25,470 in going from infinity to a distance r 125 00:07:25,470 --> 00:07:28,630 away from the planet-- I take a minus that sign. 126 00:07:28,630 --> 00:07:31,620 So the negative of the gravitational work-- 127 00:07:31,620 --> 00:07:35,390 then that's what that number corresponds to.