thesis/julia/src/mission.jl

export Phase, Mission_Guess, Mission, Bad_Mission
export test_phase1, test_phase2
export test_mg
export Vector

struct Phase
  planet::Body
  v∞_in::Vector{Float64}
  v∞_out::Vector{Float64}
  tof::Float64
  thrust_profile::Matrix{Float64}
end

const test_phase1 = Phase(Venus, [√20., -√80., 0.], [√50., -√50., 0.], 1.30464e7, zeros(20,3))
const test_phase2 = Phase(Jupiter, [0.3, 7.1, 0.2], [0.3, 7.1, 0.2], 3.9year, zeros(20,3))
const test_phases = [test_phase1, test_phase2]

"""
A convenience function for calculating mass usage given a certain thrust profile
"""
function mass_consumption(sc::Sc, phase::Phase)
  weighted_thrusting_time = 0.0
  n = size(phase.thrust_profile)[1]
  for i in 1:size(phase.thrust_profile,1)
    weighted_thrusting_time += norm(phase.thrust_profile[i,:]) * phase.tof/n
  end
  return weighted_thrusting_time*sc.mass_flow_rate
end

struct Mission_Guess
  sc::Sc
  start_mass::Float64
  launch_date::DateTime
  launch_v∞::Vector{Float64}
  phases::Vector{Phase}
  converged::Bool
end

"""
Constructor for a mission guess. Generally mission guesses are not converged
"""
function Mission_Guess(sc::Sc, mass::Float64, date::DateTime, v∞::Vector{Float64}, phases::Vector{Phase})
  # First do some checks to make sure that it's valid
  mass_used = 0
  for phase in phases
    mass_used += mass_consumption(sc, phase)
    mass - mass_used > sc.dry_mass || throw(Mass_Error(mass - mass_used))
    v∞_in, v∞_out = phase.v∞_in, phase.v∞_out
  end
  Mission_Guess(sc, mass, date, v∞, phases, false)
end

"""
This is the opposite of the function below. It takes a vector and any other necessary information and outputs a mission guess
"""
function Mission_Guess(x::Vector{Float64}, sc::Sc, mass::Float64, flybys::Vector{Body})
  # Variable mission params
  launch_date = Dates.unix2datetime(x[1])
  launch_v∞ = x[2:4]

  # Try to intelligently determine n
  three_n = ((length(x)-4)/length(flybys)) - 7
  three_n % 3 == 0 || throw(Mission_Creation_Error(three_n))
  n::Int = three_n/3

  # Build the phases
  i = 0
  phases = Vector{Phase}()
  for flyby in flybys
    phase_params = x[ 5 + (3n+7) * i : 5 + (3n+7) * (i+1) - 1 ]
    v∞_in = phase_params[1:3]
    v∞_out = phase_params[4:6]
    tof = phase_params[7]
    thrusts = reshape(phase_params[8:end], (n,3))
    push!(phases, Phase(flyby, v∞_in, v∞_out, tof, thrusts))
    i += 1
  end
  return Mission_Guess(sc, mass, launch_date, launch_v∞, phases, false)
end

"""
This is a function to convert a mission guess into an nlp-ready vector. It doesn't contain all
information from the guess though.
"""
function Base.Vector(g::Mission_Guess)
  result = Vector{Float64}()
  push!(result, Dates.datetime2unix(g.launch_date))
  push!(result, g.launch_v∞...)
  for phase in g.phases
    push!(result,phase.v∞_in...)
    push!(result,phase.v∞_out...)
    push!(result,phase.tof)
    push!(result,phase.thrust_profile...)
  end
  return result
end

function lowest_mission_vector(launch_window::Vector{DateTime}, num_phases::Int, n::Int)
  result = Vector{Float64}()
  push!(result, Dates.datetime2unix(launch_window[1]))
  push!(result, -10*ones(3)...)
  for i in 1:num_phases
    push!(result, -10*ones(3)...)
    push!(result, -10*ones(3)...)
    push!(result, 86_400.0)
    push!(result, -1 * ones(n,3)...)
  end
  return result
end

function highest_mission_vector(launch_window::Vector{DateTime}, mission_length::Float64, num_phases::Int, n::Int)
  result = Vector{Float64}()
  push!(result, Dates.datetime2unix(launch_window[2]))
  push!(result, 10*ones(3)...)
  for i in 1:num_phases
    push!(result, 10*ones(3)...)
    push!(result, 10*ones(3)...)
    push!(result, mission_length)
    push!(result, ones(n,3)...)
  end
  return result
end

const test_mg = Mission_Guess(bepi, 12_000., DateTime(1992,11,19), [-3.4,1.2,0.1], test_phases)
            
struct Mission
  sc::Sc
  start_mass::Float64
  launch_date::DateTime
  launch_v∞::Vector{Float64}
  phases::Vector{Phase}
  converged::Bool
end

"""
Constructor for a mission. Generally mission guesses are converged, so we check everything
"""
function Mission(sc::Sc, mass::Float64, date::DateTime, v∞::Vector{Float64}, phases::Vector{Phase};
                 force=false)
  # First do some checks to make sure that it's valid
  if !force
    time = date
    current_planet = Earth
    start = state(current_planet, time, v∞, mass)
    for phase in phases
      final = prop(phase.thrust_profile, start, sc, phase.tof)[2]
      mass = final[7]
      mass > sc.dry_mass || throw(Mass_Error(mass - mass_used))
      current_planet = phase.planet
      time += Dates.Second(floor(phase.tof))
      p_pos = state(current_planet, time)[1:3]
      abs(norm(final[1:3] - p_pos)) < √30_000. || throw(Planet_Match_Error(final[1:3], p_pos))
      v∞_in, v∞_out = phase.v∞_in, phase.v∞_out
      if phase != phases[end]
        abs(norm(v∞_in) - norm(v∞_out)) < 0.005 || throw(V∞_Error(v∞_in, v∞_out))
        δ = acos( ( v∞_in ⋅ v∞_out ) / ( norm(v∞_in) * norm(v∞_out) ) )
        periapsis = (phase.planet.μ/(v∞_in ⋅ v∞_in)) * ( 1/sin(δ/2) - 1 )
        periapsis > 1.1phase.planet.r || throw(HitPlanet_Error())
      end
    end
  end
  Mission(sc, mass, date, v∞, phases, true)
end

"""
BE CAREFUL!! This just makes a guess converged, whether true or not
"""
function Mission(g::Mission_Guess)
  return Mission(g.sc, g.start_mass, g.launch_date, g.launch_v∞, g.phases, force=true)
end

function Mission(x::Vector{Float64}, sc::Sc, mass::Float64, flybys::Vector{Body})
  guess = Mission_Guess(x, sc, mass, flybys::Vector{Body})
  return Mission(guess)
end

struct Bad_Mission
  message::String
  converged::Bool
end
Bad_Mission(s::String) = Bad_Mission(s,false)
Bad_Mission(s::Symbol) = Bad_Mission(String(s),false)