connor/thesis
1
0
Fork 0
Code Issues Pull Requests Actions Packages Projects Releases Wiki Activity

I think I'm pretty much at 2b now

Browse Source
This commit is contained in:
Connor
2021-09-12 19:25:40 -06:00
parent 9de9af2dde
commit e83a705e77
8 changed files with 81 additions and 60 deletions
Download Patch File Download Diff File Expand all files Collapse all files

39
julia/src/inner_loop/inner_loop.jl
View File

@@ -47,23 +47,28 @@ function inner_loop(launch_date::DateTime,
time = utc2et(Dates.format(launch_date,"yyyy-mm-ddTHH:MM:SS"))
thrust_profiles = []
for phase in phases
planet1_state = spkssb(ids[phase.from_planet], time, "J2000")
time += phase.time_of_flight
planet2_state = spkssb(ids[phase.to_planet], time, "J2000")
# TODO: Come up with improved method of calculating "n"
start = planet1_state + [0., 0., 0., phase.v∞_outgoing...]
final = planet2_state + [0., 0., 0., phase.v∞_incoming...]
if mbh_specs == nothing
best = mbh(start, final, craft, μs["Sun"], 0.0, phase.time_of_flight, 10,
verbose=verbose)[1]
else
best = mbh(start, final, craft, μs["Sun"], 0.0, phase.time_of_flight, 10,
verbose=verbose, num_iters=mbh_specs[1], patience_level=mbh_specs[2])[1]
try
for phase in phases
planet1_state = spkssb(ids[phase.from_planet], time, "J2000")
time += phase.time_of_flight
planet2_state = spkssb(ids[phase.to_planet], time, "J2000")
# TODO: Come up with improved method of calculating "n"
start = planet1_state + [0., 0., 0., phase.v∞_outgoing...]
final = planet2_state + [0., 0., 0., phase.v∞_incoming...]
if mbh_specs === nothing
best = mbh(start, final, craft, μs["Sun"], 0.0, phase.time_of_flight, 10,
verbose=verbose)[1]
else
num_iters, sil, dil = mbh_specs
best = mbh(start, final, craft, μs["Sun"], 0.0, phase.time_of_flight, 10,
verbose=verbose, num_iters=num_iters, search_patience_lim=sil,
drill_patience_lim=dil)
end
push!(thrust_profiles, best)
craft.mass = prop(tanh.(best.zero), planet1_state, sc, μs["Sun"], prop_time)[2][end]
end
push!(thrust_profiles, best)
craft.mass = prop(tanh.(best.zero), planet1_state, sc, μs["Sun"], prop_time)[2][end]
return craft.mass, thrust_profiles
catch
return "One path did not converge"
end
return craft.mass, thrust_profiles
end