Here's the scenario I use to test the launch/autopilot, etc.
It is the ISS14 supply mission of 07 Avril 2007, using ProgressPirs.
Launch at 17:31 UTC.
During the launch I use
LaunchMFD to get the initial Launch Azimuth and make correction to inclination (when you are near orbit intersection "node" with ISS).
AlignPlaneMFD to see the "time to node" (Tn).
After the launch I use
RendezvousMFD for efficient intercept of ISS.
also OrbitMFD, MapMFD, SurfaceMFD.
- Code:
-
BEGIN_DESC
Launch at 17:31 UTC. Press [P] for autopilot at T-28.
END_DESC
BEGIN_ENVIRONMENT
System Sol
Date MJD 54197.7244080092
END_ENVIRONMENT
BEGIN_FOCUS
Ship Pad LC-1
END_FOCUS
BEGIN_CAMERA
TARGET Pad LC-1
MODE Cockpit
FOV 50.00
END_CAMERA
BEGIN_HUD
TYPE Orbit
REF Earth
END_HUD
BEGIN_MFD Left
TYPE Orbit
PROJ Ship
FRAME Equator
ALT
REF Earth
TARGET ISS
END_MFD
BEGIN_MFD Right
TYPE Map
REF Earth
OTARGET ISS
ZOOM
TRACK ON
END_MFD
BEGIN_SHIPS
Pad LC-1:blc1arms
STATUS Landed Earth
POS 63.3200945 45.9123065
HEADING 90.00
END
Soyuz:M_Soyuz\Soyuz_prgpirs
STATUS Landed Earth
POS 63.3200945 45.9123065
HEADING 45.00
ATTACHED 0:0,Pad LC-1
PRPLEVEL 0:1.000 1:1.000 2:1.000
NAVFREQ 0 0
CONFIG_FILE Config\M_Soyuz\Soyuz_prgpirs.ini
GUIDANCE_FILE Config\M_Soyuz\nmauto.txt
CONFIGURATION 0
STAGE_STATE 2
STAGE_IGNITION_TIME 0.000
CURRENT_BOOSTER 1
CURRENT_STAGE 1
CURRENT_INTERSTAGE 1
CURRENT_PAYLOAD 1
FAIRING 1
END
ISS:ProjectAlpha_ISS
STATUS Orbiting Earth
RPOS -136581.43 4974950.44 -4509512.98
RVEL 5194.299 -3731.849 -4291.863
AROT 109.87 -9.79 79.95
PRPLEVEL 0:1.000
IDS 0:588 100 1:586 100 2:584 100 3:582 100 4:580 100
NAVFREQ 0 0
XPDR 466
END
END_SHIPS
BEGIN_ExtMFD
END
