Канал: Luigi Mascolo

Lecture 8 - CR3BP Lyapunov (2D) and Halo (3D) periodic orbits - generation and synodic resonance

Lecture 8 - CR3BP Lyapunov (2D) and Halo (3D) periodic orbits - generation and synodic resonance

Lecture 8 - chaotic system, lagrangian points, Jacobi constant, and zero velocity surfaces

Lecture 8 - chaotic system, lagrangian points, Jacobi constant, and zero velocity surfaces

Lecture 8 - circular restricted three body problem definition - binary systems and synodic frame

Lecture 8 - circular restricted three body problem definition - binary systems and synodic frame

Lecture 7 - inbound flyby conditions and planetocentric state evolution - missing distance

Lecture 7 - inbound flyby conditions and planetocentric state evolution - missing distance

Lecture 7 - optimal phase Earth-Mars Hohmann transfer - sphere of influence targeting

Lecture 7 - optimal phase Earth-Mars Hohmann transfer - sphere of influence targeting

Lecture 7 - geocentric rendezvous mission and heliocentric targeting for Earth-Mars transfer

Lecture 7 - geocentric rendezvous mission and heliocentric targeting for Earth-Mars transfer

Lecture 6 - second to first order differential equations for orbits in the two-body problem

Lecture 6 - second to first order differential equations for orbits in the two-body problem

Lecture 6 - ODE113 single-shooting Hohmann transfer targeting - complete ephemeris evolution

Lecture 6 - ODE113 single-shooting Hohmann transfer targeting - complete ephemeris evolution

Lecture 6 - single-shooting method for Hohmann transfer - changes in velocity and energy components

Lecture 6 - single-shooting method for Hohmann transfer - changes in velocity and energy components

Lecture 6 - velocity and energy components - ODE113 integration

Lecture 6 - velocity and energy components - ODE113 integration

Lecture 6 - in-plane and out-of-plane thrust - local coordinate frame

Lecture 6 - in-plane and out-of-plane thrust - local coordinate frame

Lecture 6 - MATLAB ODE45 vs ODE113 equations of motion integration numerical errors

Lecture 6 - MATLAB ODE45 vs ODE113 equations of motion integration numerical errors

Lecture 5 - groundtrack variation for changes in argument of periapsis and eccentricity, same period

Lecture 5 - groundtrack variation for changes in argument of periapsis and eccentricity, same period

Lecture 5 - groundtrack evolution for circular inclined orbit - variation due to RAAN changes

Lecture 5 - groundtrack evolution for circular inclined orbit - variation due to RAAN changes

Lecture 5 - geosynchronous and geostationary orbits - groundtracks

Lecture 5 - geosynchronous and geostationary orbits - groundtracks

Lecture 5 - generic groundtrack for circular inclined orbit - fixed and rotating Earth

Lecture 5 - generic groundtrack for circular inclined orbit - fixed and rotating Earth

Lecture 4 - orbit after launch for eastward kick-off, resulting inclination and circularization cost

Lecture 4 - orbit after launch for eastward kick-off, resulting inclination and circularization cost

Lecture 4 - ground station longitude and latitude, Earth rotational velocity

Lecture 4 - ground station longitude and latitude, Earth rotational velocity

Lecture 4 - real evolution of Greewich meridian per solar day - JD and MJD

Lecture 4 - real evolution of Greewich meridian per solar day - JD and MJD

Lecture 3 - three dimensional orbits - changes due to Keplerian elements variations

Lecture 3 - three dimensional orbits - changes due to Keplerian elements variations

Lecture 3 - Seasons - Heliocentric ecliptic reference frame and Greenwich right ascension at epoch

Lecture 3 - Seasons - Heliocentric ecliptic reference frame and Greenwich right ascension at epoch

Lecture 3 - Difference between solar and sidereal day - Greenwich right ascension at epoch

Lecture 3 - Difference between solar and sidereal day - Greenwich right ascension at epoch

Lecture 3 - geocentric equatorial and heliocentric ecliptic reference planes

Lecture 3 - geocentric equatorial and heliocentric ecliptic reference planes

Lecture 2 - indirect Kepler time problem - true anomaly from elapsed time

Lecture 2 - indirect Kepler time problem - true anomaly from elapsed time

Lecture 2 - direct Kepler time problem - time from true anomaly

Lecture 2 - direct Kepler time problem - time from true anomaly

Lecture 2 - planetary cosmic velocities for different central gravitational bodies

Lecture 2 - planetary cosmic velocities for different central gravitational bodies

Lecture 2 - orbital and escape velocity, closed and open orbits for different gravitational bodies

Lecture 2 - orbital and escape velocity, closed and open orbits for different gravitational bodies

Lecture 2 - cosmic velocities, orbital velocities, escape velocity, closed and open orbits

Lecture 2 - cosmic velocities, orbital velocities, escape velocity, closed and open orbits

Lecture 1 - ECI reference system, radial and tangential velocity - different gravitational bodies

Lecture 1 - ECI reference system, radial and tangential velocity - different gravitational bodies

Lecture 1 - ECI reference system, specific kinetic and potential energy

Lecture 1 - ECI reference system, specific kinetic and potential energy

Lecture 1 - ECI reference system, keplerian elements

Lecture 1 - ECI reference system, keplerian elements

NASA Space Apps Challenge - Asteroid Express Team

NASA Space Apps Challenge - Asteroid Express Team

Gemini Mars Mission - FATO Mars Team - Mission Video

Gemini Mars Mission - FATO Mars Team - Mission Video