1 00:00:03,330 --> 00:00:06,750 The little prince's asteroid B612 2 00:00:06,750 --> 00:00:10,400 is being orbited by a small body. 3 00:00:10,400 --> 00:00:12,360 It has a mass m. 4 00:00:12,360 --> 00:00:21,840 And it goes around this asteroid B612 that has a mass m1. 5 00:00:21,840 --> 00:00:23,520 We should add a coordinate system. 6 00:00:23,520 --> 00:00:29,140 We always know about r-hat goes radially outward. 7 00:00:29,140 --> 00:00:31,800 And we know from the universal law of gravitation 8 00:00:31,800 --> 00:00:34,470 that we have mutual attraction between these bodies. 9 00:00:34,470 --> 00:00:38,255 And actually, that's going to point inward. 10 00:00:38,255 --> 00:00:41,060 And because we're having orbital motion here, 11 00:00:41,060 --> 00:00:44,020 so circular motion, the acceleration, 12 00:00:44,020 --> 00:00:45,840 the radial component of the acceleration 13 00:00:45,840 --> 00:00:49,260 will also point inward. 14 00:00:49,260 --> 00:00:54,320 We need to consider all of that for our f equals ma analysis 15 00:00:54,320 --> 00:00:59,000 that we are going to do now, because the little prince wants 16 00:00:59,000 --> 00:01:05,510 to know how far this little body is away from his asteroid. 17 00:01:05,510 --> 00:01:11,450 So we have the gravitational universal law here, 18 00:01:11,450 --> 00:01:19,090 minus Gmm1 over the distance squared. 19 00:01:19,090 --> 00:01:21,950 So the distance here between the two planets, 20 00:01:21,950 --> 00:01:25,400 r, which is what we want to calculate. 21 00:01:25,400 --> 00:01:29,890 And then we have over here for circular motion, 22 00:01:29,890 --> 00:01:34,720 the description of mr omega squared. 23 00:01:34,720 --> 00:01:37,700 Now, the little prince can't measure omega. 24 00:01:37,700 --> 00:01:41,100 But the little prince has a little time clock. 25 00:01:41,100 --> 00:01:45,130 So what he can measure is the period from here 26 00:01:45,130 --> 00:01:48,520 until he sees the body again. 27 00:01:48,520 --> 00:01:52,200 And that is 2pi over omega. 28 00:01:52,200 --> 00:01:55,145 So we can add that in here. 29 00:01:55,145 --> 00:02:02,120 mr 4pi squared over T squared. 30 00:02:02,120 --> 00:02:07,335 And this m here will cancel out. 31 00:02:07,335 --> 00:02:10,169 And we have to solve this for r. 32 00:02:10,169 --> 00:02:12,240 What we're going to see-- 33 00:02:12,240 --> 00:02:14,160 Oh and of course, we have a minus sign 34 00:02:14,160 --> 00:02:18,460 here because in the life of the little prince, 35 00:02:18,460 --> 00:02:21,250 of course gravitational acceleration 36 00:02:21,250 --> 00:02:22,480 is not going outwards. 37 00:02:22,480 --> 00:02:26,890 It's going inward, so we better give this a minus here and here 38 00:02:26,890 --> 00:02:28,130 as well. 39 00:02:28,130 --> 00:02:30,490 And we will actually see that that then 40 00:02:30,490 --> 00:02:32,090 cancels out against this one. 41 00:02:32,090 --> 00:02:34,460 And we're going to solve this for r. 42 00:02:34,460 --> 00:02:38,920 So we get r cubed, actually. 43 00:02:38,920 --> 00:02:47,340 And then we have Gm1 over 4pi squared. 44 00:02:47,340 --> 00:02:50,540 And here, we have T squared. 45 00:02:50,540 --> 00:02:59,950 And you can also just write that as Gm1 or pi squared T squared. 46 00:02:59,950 --> 00:03:06,640 And then we have third root. 47 00:03:06,640 --> 00:03:09,590 So you might have seen this equation here. 48 00:03:09,590 --> 00:03:11,480 This is actually Kepler's law. 49 00:03:11,480 --> 00:03:15,240 It describes the motion of the planets around the sun. 50 00:03:15,240 --> 00:03:17,640 Well, it really only does it if the motions 51 00:03:17,640 --> 00:03:18,970 are fairly circular. 52 00:03:18,970 --> 00:03:22,970 For elliptical orbits, it is not such a good approximation, 53 00:03:22,970 --> 00:03:27,480 although Kepler derived it like that quite a while ago. 54 00:03:27,480 --> 00:03:29,329 And that was really an astonishing result. 55 00:03:29,329 --> 00:03:31,690 So here, we have this again that the cube 56 00:03:31,690 --> 00:03:33,900 of the distance between two objects 57 00:03:33,900 --> 00:03:38,280 is proportional to the square of the period of the orbiting 58 00:03:38,280 --> 00:03:39,829 time.