diff options
Diffstat (limited to 'src/main.py')
| -rw-r--r-- | src/main.py | 20 |
1 files changed, 10 insertions, 10 deletions
diff --git a/src/main.py b/src/main.py index 08c6229..5b6f673 100644 --- a/src/main.py +++ b/src/main.py @@ -99,7 +99,7 @@ def main(argv): simulation.tick(delta=delta) #TODO: draw body sprite, rocket sprite, clouds sprites, etc. - #TODO: implement height properly (body radius) + actually implement body + #TODO: implement gravity properly (x and y) #TODO: do max load on rocket so it blows up #TODO: allow multilanguage api for landing algorithms etc @@ -135,15 +135,15 @@ def draw_simulation(simulation_display: type[pygame.Surface], simulation: type[S curr_thrust = simulation.rocket.current_stage().current_thrust(g, simulation.heading) simulation_display.blit(font.render("Simulation time: {:.0f}s".format(simulation.time), False, (255, 255, 255)),(0,0)) - simulation_display.blit(font.render("X: {:.0f}m".format(simulation.x), False, (255, 255, 255)),(0,40)) - simulation_display.blit(font.render("Y: {:.0f}m".format(simulation.y), False, (255, 255, 255)),(0,80)) - simulation_display.blit(font.render("Speed x: {:.0f}m/s".format(simulation.speed_x), False, (255, 255, 255)),(0,120)) - simulation_display.blit(font.render("Speed y: {:.0f}m/s".format(simulation.speed_y), False, (255, 255, 255)),(0,160)) - simulation_display.blit(font.render("Acceleration x: {:.2f}m/s2".format(simulation.acceleration_x), False, (255, 255, 255)),(0,200)) - simulation_display.blit(font.render("Acceleration y: {:.2f}m/s2".format(simulation.acceleration_y), False, (255, 255, 255)),(0,240)) - simulation_display.blit(font.render("Thrust x: {:.0f}N".format(simulation.rocket.current_stage().current_thrust(g, simulation.heading)[0]), False, (255, 255, 255)),(0,280)) - simulation_display.blit(font.render("Thrust y: {:.0f}N".format(simulation.rocket.current_stage().current_thrust(g, simulation.heading)[1]), False, (255, 255, 255)),(0,320)) - simulation_display.blit(font.render("Altitude: {:.0f}m".format(simulation.rocket_altitude()), False, (255, 255, 255)),(0,360)) + simulation_display.blit(font.render("Altitude: {:.0f}m".format(simulation.rocket_altitude()), False, (255, 255, 255)),(0,40)) + simulation_display.blit(font.render("X: {:.0f}m".format(simulation.x), False, (255, 255, 255)),(0,80)) + simulation_display.blit(font.render("Y: {:.0f}m".format(simulation.y), False, (255, 255, 255)),(0,120)) + simulation_display.blit(font.render("Speed x: {:.0f}m/s".format(simulation.speed_x), False, (255, 255, 255)),(0,160)) + simulation_display.blit(font.render("Speed y: {:.0f}m/s".format(simulation.speed_y), False, (255, 255, 255)),(0,200)) + simulation_display.blit(font.render("Acceleration x: {:.2f}m/s2".format(simulation.acceleration_x), False, (255, 255, 255)),(0,240)) + simulation_display.blit(font.render("Acceleration y: {:.2f}m/s2".format(simulation.acceleration_y), False, (255, 255, 255)),(0,280)) + simulation_display.blit(font.render("Thrust x: {:.0f}N".format(simulation.rocket.current_stage().current_thrust(g, simulation.heading)[0]), False, (255, 255, 255)),(0,320)) + simulation_display.blit(font.render("Thrust y: {:.0f}N".format(simulation.rocket.current_stage().current_thrust(g, simulation.heading)[1]), False, (255, 255, 255)),(0,360)) simulation_display.blit(font.render("Fuel in stage: {:.0f}kg".format(simulation.rocket.current_stage().fuel_mass), False, (255, 255, 255)),(0,400)) simulation_display.blit(font.render("Stage mass: {:.0f}kg".format(simulation.rocket.current_stage().total_mass()), False, (255, 255, 255)),(0,440)) simulation_display.blit(font.render("Rocket mass: {:.0f}kg".format(simulation.rocket.total_mass()), False, (255, 255, 255)),(0,480)) |