X Y Z r V o P O a  C s X Y Z r V o P O a  C s unun utut.

Slides:



Advertisements
Similar presentations
XII - Standard Mathematics
Advertisements

MAE 5410 – Astrodynamics Lecture 5 Orbit in Space Coordinate Frames and Time.
GN/MAE155B1 Orbital Mechanics Overview 2 MAE 155B G. Nacouzi.
Space Engineering I – Part I
ARO309 - Astronautics and Spacecraft Design Winter 2014 Try Lam CalPoly Pomona Aerospace Engineering.
Particle vs. Rigid-Body Mechanics
Slide 0 SP200, Block III, 1 Dec 05, Orbits and Trajectories UNCLASSIFIED The Two-body Equation of Motion Newton’s Laws gives us: The solution is an orbit.
What’s the difference? What to choose. By Jordan Lyford Group: Ground Station.
Basic Circuit Elements Note: Keep grid snap on, this helps align devices on nodes All devices are sized to fit the default grid F1F1 V1V1 I1I1 Q 23 M 23.
Kepler. Inverse Square Force  Force can be derived from a potential.  < 0 for attractive force  Choose constant of integration so V (  ) = 0. m2m2.
What are ground tracks? COE Determination a e i   ? ? ? ? ? ? COE Determination.
Colorado Center for Astrodynamics Research The University of Colorado 1 Computation of Azimuth and Elevation George H. Born These slides describe how to.
Analytic Geometry Section 3.3
Central Forces. Two-Body System  Center of mass R  Equal external force on both bodies.  Add to get the CM motion  Subtract for relative motion m2m2.
R F For a central force the position and the force are anti- parallel, so r  F=0. So, angular momentum, L, is constant N is torque Newton II, angular.
Math 143 Section 7.1 The Ellipse
GN/MAE155A1 Orbital Mechanics Overview MAE 155A Dr. George Nacouzi.
Orbital Mechanics Overview
Satellite Orbits 인공위성 궤도
Chpt. 5: Describing Orbits By: Antonio Batiste. If you’re flying an airplane and the ground controllers call you on the radio to ask where you are and.
Orbital Characteristics of Megha-Tropiques T.Ravindra Babu M.S.Jayashree G.Raju ISRO Satellite Centre Bangalore.
COMETS, KUIPER BELT AND SOLAR SYSTEM DYNAMICS Silvia Protopapa & Elias Roussos Lectures on “Origins of Solar Systems” February 13-15, 2006 Part I: Solar.
Morehead State University Morehead, KY Prof. Bob Twiggs Understanding Orbits Orbit Facts 1.
ORBITAL MECHANICS: HOW OBJECTS MOVE IN SPACE FROM KEPLER FIRST LAW: A SATELLITE REVOLVES IN AN ELLIPTICAL ORBIT AROUND A CENTER OF ATTRACTION POSITIONED.
Section 7.1 – Conics Conics – curves that are created by the intersection of a plane and a right circular cone.
Introduction to Satellite Motion
AT737 Satellite Orbits and Navigation 1. AT737 Satellite Orbits and Navigation2 Newton’s Laws 1.Every body will continue in its state of rest or of uniform.
Phases of the Moon. Spin and orbital frequencies.
ASEN 5050 SPACEFLIGHT DYNAMICS Two-Body Motion Prof. Jeffrey S. Parker University of Colorado – Boulder Lecture 3: The Two Body Problem 1.
SLS-RFM_14-18 Orbital Considerations For A Lunar Comm Relay
Coriolis Effect on the spinning Earth. Trajectories inertial reference frame.
A Brief Introduction to Astrodynamics
Albireo: The Boy Scout star Chapter 5: Binary stars and stellar masses.
Conic Sections in Polar Coordinates Lesson Definition of Parabola Set of points equal distance from a point and a line  Point is the focus 
ASTROPHYSICS Yr 2 Session 3 – Orbits & the Solar System 1.
& & & Formulas.
Chapter 5 Satellite orbits Remote Sensing of Ocean Color Instructor: Dr. Cheng-Chien LiuCheng-Chien Liu Department of Earth Science National Cheng-Kung.
10.2 The Parabola. A parabola is defined as the locus of all points in a given plane that are the same distance from a fixed point, called the focus,
9.2 THE PARABOLA. A parabola is defined as the collection of all points P in the plane that are the same distance from a fixed point F as they are from.
10.2 The Parabola. A parabola is defined as the collection of all points P in the plane that are the same distance from a fixed point F as they are from.
“Backwards” Parabolas Today you will write the equation of a parabola given defining characteristics or the graph.
Earth and Moon in Space.
Elliptical Orbit perigee moon The moon travels about Earth in an elliptical orbit with Earth at one focus. Find the greatest and smallest distances (the.
, Moon, Sun System. Moon “appears” to go around from E W ` Really, rotates below it.
ASEN 5070: Statistical Orbit Determination I Fall 2014
Chapter 12 KINETICS OF PARTICLES: NEWTON’S SECOND LAW Denoting by m the mass of a particle, by  F the sum, or resultant, of the forces acting on the.
AGBell -1- Build the A Train Constellation using STK Next we will use global information about the Earth to help define and understand how the A-Train.
Conic Sections.
What am I?. x 2 + y 2 – 6x + 4y + 9 = 0 Circle.
Conics: Parabolas. Parabolas: The set of all points equidistant from a fixed line called the directrix and a fixed point called the focus. The vertex.
Categories of Satellites
University of Colorado Boulder ASEN 5070: Statistical Orbit Determination I Fall 2015 Professor Brandon A. Jones Lecture 2: Basics of Orbit Propagation.
More Conic Sections. Objective Given a translation, I can graph an equation for a conic section.
Learning from the Past, Looking to the Future James R. (Jim) Beaty, PhD - NASA Langley Research Center Vehicle Analysis Branch, Systems Analysis & Concepts.
Hyperbolas Date: ______________. Horizontal transverse axis: 9.5 Hyperbolas x 2x 2 a2a2 y2y2 b2b2 –= 1 y x V 1 (–a, 0)V 2 (a, 0) Hyperbolas with Center.
AE Review Orbital Mechanics.
PHYS 2006 Tim Freegarde Classical Mechanics. 2 Newton’s law of Universal Gravitation Exact analogy of Coulomb electrostatic interaction gravitational.
Space Mechanics.
EE 495 Modern Navigation Systems
SLS-RFM_14-18 Orbital Considerations For A Lunar Comm Relay
Dynamics Dynamics Rotational K.E. Tides g as a function of latitude
22.2 – The Earth-Moon-Sun System – Part II
Conic Sections in Polar Coordinates
Orbit in Space Coordinate Frames and Time
Next we will use global information about the Earth to help define and understand how the A-Train orbits the Earth.
Section 10.2 Ellipses.
A e i o u.
Earth, sun and moon.
Seasons.
Conics Review.
Presentation transcript:

X Y Z r V o P O a  C s X Y Z r V o P O a  C s unun utut

FgFg m M r FgFg FgFg m M r FgFg FgFg m M r FgFg

X Y Z r m O FgFg X Y Z r V m P O F net

X Y Z r m O FgFg X Y Z r V m P O

X Y Z r V m P O r X Y Z O X’ Y’ Z’ O ’ Inertial frame Moving frame

M m X Y Z O X’ Y’ Z’ M m X Y Z O X’ Y’ Z’ FgFg FgFg rMrM rMrM rmrm rmrm r r

Q X Y Z i j k Inertial frame Moving frame P X Y Z x y z Inertial frame Moving frame o O r roro r rel

X Greenish meridian Y Z x’ y z’ P z y’ x Λ θgθg  r rel o Equator Earth axis of rotation

X Y Z R1R1 O R2R2 RGRG G r m1m1 m2m2 m2m2 m1m1 F 12 F 21 m1m1 m2m2 r m1m1 m2m2 r v vrvr vv m1m1 m2m2 r e 

O f b B f rprp rara rBrB  r r+dr f  Apse line v vrvr vv  = / 2 = / 2

f Perigee S/C 

f Perigee Ellipse focus Line of nodes  f Periapsis Latus rectum P

Z Y X Perigee Node line  e Earth’s north polar axis S/C v r Ascending node Earth’s equatorial plane  h   i

r v vrvr vv  Periapse f Semilatus rectum

F F’ A P C   aa |ra||ra| rprp I II  b M  Asymptote Apse line Empty focus Vacant orbit

O f b 11 a 22 ae