Earth Centered Inertial (ECI) Frame

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Related lectures (31)

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True Anomaly in Elliptical Orbits

Explores true anomaly in elliptical orbits and the transformation between Cartesian and polar coordinates.

Crew-7 Return and Space Mission Design Overview

Discusses Crew-7's return from the ISS and key principles of space mission design.

Nodal Regression and Sun-synchronous Orbits

Explores nodal regression, forces in LEO, and Sun-synchronous orbits.

Kepler Laws and Anomalies

Covers the determination of satellite vehicle coordinates with respect to Earth using almanac and ephemerides.

Space Mission Design: Starship Test and Rendezvous Techniques

Discusses SpaceX's Starship test flight and the principles of rendezvous in space missions.

Earth-Centered-Earth-Fixed (ECEF) Frame

Explores the ECEF frame for satellite positions, orbital planes, and orbit parameters.

Orbital Parameters and Calendars

Explains classical orbital parameters, spacecraft's state vector, and Gregorian vs. Julian days.

Kepler's Laws and Orbital Mechanics

Explores Kepler's laws, orbital mechanics, energy of motion, flight path angles, orbital maneuvers, Hohmann transfers, geostationary orbits, and Lagrange points.

Space Mission Design and Operations

Covers space mission design, spacecraft energy, orbits, and maneuvers, including gravity effects, tethers, and interplanetary trajectories.

Interplanetary Trajectories: Orbital Characteristics

Covers interplanetary trajectories, sphere of influence, and orbital characteristics of planets.