A e i o u.

Slides:



Advertisements
Similar presentations
The Important Thing About By. The Important Thing About ******** The important thing about ***** is *****. It is true s/he can *****, *****, and *****.
Advertisements

MAE 5410 – Astrodynamics Lecture 5 Orbit in Space Coordinate Frames and Time.
Introduction to RINEX, GPS Raw Data
GN/MAE155B1 Orbital Mechanics Overview 2 MAE 155B G. Nacouzi.
Dr. Andrew Ketsdever Lesson 3 MAE 5595
Space Engineering I – Part I
ARO309 - Astronautics and Spacecraft Design Winter 2014 Try Lam CalPoly Pomona Aerospace Engineering.
ECE 5233 Satellite Communications
Orbital Aspects of Satellite Communications
Introduction to Orbital Mechanics
Prince William Composite Squadron Col M. T. McNeely Presentation for AGI Users Conference CIVIL AIR PATROL PRESENTS The CAP-STK Aerospace Education Program.
Colorado Springs Cadet Squadron Lt Col M. T. McNeely Orbital Mechanics and other Space Operations Topics !! CIVIL AIR PATROL CAP-STK Aerospace Program.
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 are ground tracks? COE Determination a e i   ? ? ? ? ? ? COE Determination.
Basic Orbital Mechanics Dr. Andrew Ketsdever MAE 5595.
Physics 681: Solar Physics and Instrumentation – Lecture 18 Carsten Denker NJIT Physics Department Center for Solar–Terrestrial Research.
Dynamics I 15-nov-2006 E. Schrama If there is one thing that we understand very well about our solar system, then it is the way.
1 Satellite observation systems and reference systems (ae4-e01) Orbit Mechanics 1 E. Schrama.
Numerical Simulations of the Orbits for Planetary Systems: from the Two-body Problem to Orbital Resonances in Three-body NTHU Wang Supervisor Tanigawa,
5.2 Computing Orbiting Elements
Satellite Orbits 인공위성 궤도
Presented by Rehana Jamal (GIS Expert & Geographer) Dated: Advance Applications of RS/GIS in Geo-Environmental Conservation Subject Lecture-6.
The true orbits of visual binaries can be determined from their observed orbits as projected in the plane of the sky. Once the true orbit has been computed,
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.
Satellite Orbits and Navigation 2
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.
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.
Sub-Optimal Solutions for Satellite Orbital Transfers 6th International Workshop and Advanced School 6th International Workshop and Advanced School "Spaceflight.
1 Satellite orbits. Where is the satellite ? May we see it ? Satellite geophysics,
The true orbits of visual binaries can be determined from their observed orbits as projected in the plane of the sky. Once the true orbit has been computed,
CAP-STK Aerospace Program
University of Colorado Boulder ASEN 5070: Statistical Orbit Determination I Fall 2014 Professor Brandon A. Jones Lecture 3: Basics of Orbit Propagation.
A SATELLITE CONSTELLATION TO OBSERVE THE SPECTRAL RADIANCE SHELL OF EARTH Stanley Q. Kidder and Thomas H. Vonder Haar Cooperative Institute for Research.
A Brief Introduction to Astrodynamics
General Motion Rest: Quasars Linear: Stars Keplerian: Binary Perturbed Keplerian: Asteroids, Satellites Complex: Planets, Space Vehicles Rotational: Earth,
Chapter 5 Satellite orbits Remote Sensing of Ocean Color Instructor: Dr. Cheng-Chien LiuCheng-Chien Liu Department of Earth Science National Cheng-Kung.
Space platform and Orbits Introduction to Remote Sensing Instructor: Dr. Cheng-Chien LiuCheng-Chien Liu Department of Earth Sciences National Cheng Kung.
Spheroidal Coordinates
UNCLASSIFIEDUNCLASSIFIED Lesson 2 Basic Orbital Mechanics A537 SPACE ORIENTATION A537 SPACE ORIENTATION.
ASEN 5070: Statistical Orbit Determination I Fall 2014
ASEN 5050 SPACEFLIGHT DYNAMICS Two-Body Motion Prof. Jeffrey S. Parker University of Colorado – Boulder Lecture 3: The Two Body Problem 1.
Sea Launch/Zenit Thrust: 8,180,000 N Fueled Weight: 450,000 kg Payload to LEO: 13,740 kg Cost per launch: $100,000,000 Cost per kg: $7,300 Launches: 31/28.
AS 3004 Stellar Dynamics Energy of Orbit Energy of orbit is E = T+W; (KE + PE) –where V is the speed in the relative orbit Hence the total Energy is is.
Latitude & Longitude Practice
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.
Colorado Springs Cadet Squadron Lt Col M. T. McNeely ORBITAL MECHANICS !! INTRO TO SPACE COURSE.
Introduction to satellite orbits Carla Braitenberg Si ringrazia: Peter Wisser, Delft University Monitoraggio Geodetico e Telerilevamento
Celestial Mechanics III
AE Review Orbital Mechanics.
Aircraft Communication Type 1Satellites and radars AUL-Jadra.
Deployment Optimization for Various Gravitational Wave Missions
Space Mechanics.
The Global Positioning System
Astronomy 340 Fall 2005 Class #3 13 September 2005.
LRO Mission Baseline Ephemeris v10.0
Satellite Orbits An Introduction to Orbital Mechanics
Basic Orbital Mechanics
به نام خدا تعیین مدار.
Scale: Kilometers.
Orbit in Space Coordinate Frames and Time
Longitude and Latitude
Rotational Kinematics
PROBA 2 orbits and conditions of EUV observations V. Slemzin P. N
Chapter 2. Orbits and Launching Methods
Scale: Kilometers.
Latitude & Longitude Practice
Presentation transcript:

a e i o u

a e i   u

a e i   

a e i   

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

k ^ j ^ i ^

k ^ j ^ i ^

k ^ j ^ i ^

j ^ k ^ i ^

j ^ k ^ i ^

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

j ^ k ^ i ^

j ^ k ^ i ^

j ^ k ^ i ^

j ^ k ^ i ^

j ^ k ^ i ^

j ^ k ^ i ^

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

j ^ k ^ i ^

k ^ j ^ i ^

k ^ j ^ i ^

k ^ i ^ j ^

k ^ i ^ j ^

k ^ i ^ j ^

k ^ i ^ j ^

k ^ h i ^ j ^

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

k ^ h i ^ j ^

k ^ h j ^ i ^

k ^ h j ^ i ^

k ^ h j ^ i ^

k ^ h j ^ i ^

k ^ h j ^ i ^

k ^ h n j ^ i ^

k ^ h n j ^ i ^

k ^ h n j ^ i ^

k ^ h j ^ i ^ n

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

k ^ h j ^ i ^ n

k ^ j ^ h n i ^

k ^ j ^ h n i ^

k ^ j ^ h n i ^

k ^ j ^ h n i ^

k ^ j ^ h n i ^

k ^ j ^ e h n i ^

k ^ e j ^ h n i ^

e k ^ j ^ h n i ^

k ^ e j ^ h n i ^

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

k ^ e j ^ h n i ^

a e i    semimajor axis eccentricity inclination right ascension of the ascending node  argument of perigee  true anomaly

Alternate COEs  u l longitude of perigee argument of latitude true longitude

k ^ e j ^ h n i ^