MATLAB AEROSPACE TOOLBOX RELEASE NOTE Manuale Utente Scaricare il pdf (Pagina 14)

R2015a

1-2

Earth-centered inertial to azimuth, elevation, and range block

The ECI Position to AER block calculates azimuth, elevation, and slant range coordinates

for Earth-centered inertial position.

Additional ephemerides coefficient support for celestial phenomena

blocks

The Planetary Ephemeris and Moon Libration blocks now support the DE432t

ephemerides database.

New World Magnetic Model 2015 block

The World Magnetic Model 2015 block implements the world magnetic model for years

2015 to 2020 (WMM-2015).

Updated Example

The NASA HL-20 with Optional FlightGear Interface example has been updated to take

advantage of Simulink

Projects.

1 2 ... 9 10 11 12 13 14 15 16 17 18 19 ... 77 78

Nessun commento

MATLAB AEROSPACE TOOLBOX RELEASE NOTE Manuale Utente Pagina 14