sshilovsky / kos-career Goto Github PK

want ability to launch multiple probes with different missions on one vehicle. E.g. polar comsats together with high-atm contract probe.

mission stages:

• booting vehicle with booster script to low orbit.
• when booster is depleted (or max apoapsis achieved for plane), load each probe with the same script to boost and circularize into low orbit.
• align panels to sun.
• next stage script can be loaded manually.

• don't add alarms to the past. this can happen due to 60s margin before
  maneuver node.
• find why align_solar points to either north or south. that's weird
• iterative update for alarms
• removing alarms. some owner-specific #ids might be used
• try to keep 1.8 twr after 32000k; decrease pitch maneuver starting speed;
  increase 32000k border to 35k
• try WAIT to synchronize hasnode/nextnode/remove operations
• keep suborbital insertion related data in file on volume 0: list of ship names and/or their align status
• iterative sync; fix sync errors
• remove TODOs from comsat script and move them here

as we can calculate circularization burn length, it's now possible to stop suborbital insertion as soon as we have enough time above atm to circularize.

probably it might worth it to account for changing isp when staging

• align_solar() should identify type, number and direction of panels available
• lock_steering(vector) should try to roll so that the solar panel area is maximized

• don't add alarms to the past. this can happen due to 60s margin before
  maneuver node.
• find why align_solar points to either north or south. that's weird
• iterative update for alarms
• removing alarms. some owner-specific #ids might be used
• try to keep 1.8 twr after 32000k; decrease pitch maneuver starting speed;
  increase 32000k border to 35k
• try WAIT to synchronize hasnode/nextnode/remove operations
• keep suborbital insertion related data in file on volume 0: list of ship names and/or their align status
• iterative sync; fix sync errors
  • use improved precision mean_anomaly
  • probably move (re)sync code into volume 0 domain.
• migrate modern library functions into comsat's minilib
• remove TODOs from comsat script and move them here

find some more reliable condition to check achieve desired pitch angle during gravity turn initiation