hmm... ok, here's the deal...
i'm now programming for the engine staging operations on my G42 Starliner....
as for simulating engine dynamics, i've got that covered, as far as flight envelope reaction goes:hmm:
but i've struck a new complication....
i have two different sets of engines, and four different configurations
the two pair of nozzles are located on distinct points of the airframe... enough to cause a simulation-worthy flight dynamics change.....
and another, the first set of engines should be a rocketturbine concept, which implies a bit of a delay between the controls and engine response...
for calculating the delay, i'll just us my simple smoothing formula, that uses a delta-percent-per-step addition... it's quite simple and proven....
but simple as it is, it needs one thing... INPUT:facepalm:
and i'm having heaps of trouble separating the main engine input from response
i need some ideas on how to approach this...
my first idea, which i don't know why failed, was to use a "virtual thruster group"... i created a group, passed NULL for the thruster array, and it to THGROUP_MAIN.....
then i used my simple filter formula to bridge this virtual thgroup to the actual thrusters, now grouped under THGROUP_USER
booyah, nothing....:facepalm:
i thought i had something mistaken on my end, as most often is the case, but after a brief series of tests i found i was getting no input whatsoever from the virtual thrusters - GetThrusterGroupevel() was returning a solid zero
what need i do?
i'm now programming for the engine staging operations on my G42 Starliner....
as for simulating engine dynamics, i've got that covered, as far as flight envelope reaction goes:hmm:
but i've struck a new complication....
i have two different sets of engines, and four different configurations
the two pair of nozzles are located on distinct points of the airframe... enough to cause a simulation-worthy flight dynamics change.....
and another, the first set of engines should be a rocketturbine concept, which implies a bit of a delay between the controls and engine response...
for calculating the delay, i'll just us my simple smoothing formula, that uses a delta-percent-per-step addition... it's quite simple and proven....
but simple as it is, it needs one thing... INPUT:facepalm:
and i'm having heaps of trouble separating the main engine input from response
i need some ideas on how to approach this...
my first idea, which i don't know why failed, was to use a "virtual thruster group"... i created a group, passed NULL for the thruster array, and it to THGROUP_MAIN.....
then i used my simple filter formula to bridge this virtual thgroup to the actual thrusters, now grouped under THGROUP_USER
booyah, nothing....:facepalm:
i thought i had something mistaken on my end, as most often is the case, but after a brief series of tests i found i was getting no input whatsoever from the virtual thrusters - GetThrusterGroupevel() was returning a solid zero
what need i do?
