qtrocket2/docs/flight_sequence.puml
2025-04-20 12:29:36 -06:00

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@startuml
participant "FlightSimulator" as FS
participant "Rocket" as Rocket
participant "Stage" as Stage
participant "Motor" as Motor
participant "ForcesModel" as FM
participant "Environment" as Env
participant "Integrator" as Integrator
participant "FlightState" as State
participant "RecoverySystem" as Recovery
== Launch Preparation ==
FS -> Rocket: prepareForFlight(environment)
== Launch Simulation ==
loop simulation time steps
FS -> Stage: updateMotors(deltaTime)
FS -> FM: computeNetForce(State)
FM -> Rocket: query mass/CG
FM -> Env: get air density, gravity
FM -> Motor: get thrust
FS -> Integrator: step(State, netForce, deltaTime)
Integrator -> Rocket: query mass
FS -> Rocket: applyFlightState(State)
alt FS -> Rocket: check for burnout, apogee, recovery deployment
Rocket -> RecoverySystem: checkDeploymentCondition
end
== Landing ==
FS -> FlightState: detect low altitude and low vertical velocity
note over FS
End simulation after landing detected
end note
@enduml