Vizzy program to enter geostationary orbit

Channel:
Michael Lundgren
Subscribers:
1,250
Published on ● Video Link: https://www.youtube.com/watch?v=TVeXVvXSCiI


Duration: 1:54
74 views
7

It starts from a low parking orbit of 132km AGL and waits to perform the burn so it reaches apoapsis at the exact time when it will be over the Space Center. Then it circularizes at apoapsis 8,804km AGL with a focus on making sure the orbital period is exactly 14 hours.



Other Videos By Michael Lundgren


2021-06-05Vizzy Maneuver Node
2021-06-03Vizzy Automated Handrew's Comet Intercept
2021-06-03Hyperbolic trajectory timewarp bug
2021-06-02Vizzy controlled Precision Burn on main engine (2 second wind down)
2021-06-02Vizzy Burn Node tests
2021-05-24I calculated my predicted position vector from 35 million meters out and passed within 35 meters.
2021-05-23Calculating orbital position through 2 SOI changes based on starting conditions.
2021-05-23Calculating future orbital position of periapsis during a SOI change
2021-05-23Calculating SOI enter time with Vizzy
2021-05-12Geostationary craft viewed from the ground.
2021-05-11Vizzy program to enter geostationary orbit
2021-04-13MFD Filled Polygon
2021-04-12MFD Filled triangle
2021-04-04Perfect Circular Orbit
2021-04-03Combining N-body with 50% Elastic collisions
2021-04-032D Particle Simulation
2021-04-03MFD Elastic Collisions
2021-04-02N body physics simulation MFD
2021-03-26Vizzy Police Siren
2021-03-25Asteroid can now collide and bounce off each other
2021-03-25Asteroids implemented. Collisions not done yet