Lecture 13B
Networking
Internet Basics
IP - Datagrams
TCP - UDP
Application Layer
Ports
Java Networking
URL
InetAddress
Sockets
Client-Server

RMI
Exercises

Lectures

1A: Introduction
1B: Java Intro
2A: BuildingBlocks
2B: Objects
3A: More Objects
3B: Exceptions
       & Threads
4A: Waves
4B: Nuclear &
       Particle
5A: AWT
5B: More AWT
      & Graphics
6A:Detectors &
      Simulation
6B: LHC/Atlas &
     RandomSims    
7A: Swing
7B: Java2D
8A: Java Apps
8B: Dialogs &
    MoreClasses
9A: Java I/O
9B: Utilities,
        Unicode
10A: More
    Threading
10B: File
    Handling
11A: Array,Print,
    Images
11B: SimplePhysics
    Simulation
12A: Tips &
    Techniques
12B: More Tips &
    Techniques
13A: Satellite
    
Simulations
13B: Intro to Java
    Networking
14A: Java Servers
14B: HTTP Server
15A: ServerClient
15B: ServerClient
   Expt.Simulation
16A: Course
          Review
16B: ExerciseTest
        Discussion

    Contacts
    Description
    Exercises
    Index
    Outline
    Q&A
    Resources
    StudentInfoForm
    Student Pages
    What's New

 

Home : Lectures : Lecture 13B Title Page
Lecture 13B: Introduction to Java Networking

NASA's Observatorium

Kepler's Three Laws of Planetary Motion

Law 3: The squares of the planets' orbital periods are proportional
to the cubes of the semimajor axes of their orbits.


orbit3.java

Kepler's third law is illustrated for circular orbits, although the law also applies to elliptical orbits. Click on either of the buttons on the right. The satellite's motion will simulate either the orbit of NASA's space shuttle or that of a satellite in a geosynchronous orbit. A geosynchronous orbit is one with an orbital period equal to the period of the rotation of the Earth. This means that for circular orbits above the Earth's equator, the satellite will always remain above the same point on the Earth.

You can also click on the satellite and drag it to other orbits. The satellite's altitude above the Earth's surface and orbital period are given on the right.

Notice how much slower the satellite moves in a large orbit, and how much longer it takes to complete an orbit than when it is closer to the Earth. A mathematical relationship exists between the orbital period and the size of the orbit, i.e., the distance between the center of the Earth and the satellite. The relationship states that the square of the orbital period is proportional to the cube of the size of the orbit.

Comments to: Observatorium Curator (curator@rspac.ivv.nasa.gov)

Copyright © 1995-1998 BDM Federal, Inc. All rights reserved (with exceptions noted).

 

 

 

 

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Physics Simulations with JavaTM
KTH, Kurskod: 5A1418
Curator: Clark S. Lindsey