Problem3_17

Problem3_17 - % Austin Jones % CVEN 302-501, Spring 2011 %...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
% PORGRAM Problem3_17.m % % This program solves problem 3.17 in Chapman (2008). % Refraction % % Define Variables: % r - distance from the center of the earth % theta - angle from the center of the earth % e - eccentricy of orbit % p - parameter defining the size of the size of the orbit
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: % Austin Jones % CVEN 302-501, Spring 2011 % p=1000; p e=input('value for eccentricy of orbit:\n'); theta=0:.01:2*pi; r=p./(1-e.*cos(theta)); polar(theta,r); max_radius=max(r) min_radius=min(r) m...
View Full Document

This note was uploaded on 03/03/2011 for the course CVEN 302 taught by Professor Edge during the Spring '08 term at Texas A&M.

Ask a homework question - tutors are online