ENH: Moved Flight prints to flight_prints.py

[MateusStano]

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• Code base additions (bugfix, features)
• Code maintenance (refactoring, formatting, renaming, tests)
• ReadMe, Docs and GitHub maintenance
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Pull request checklist

Please check if your PR fulfills the following requirements, depending on the type of PR:

• Tests for the changes have been added

• Docs have been reviewed and added / updated if needed

• Lint (black rocketpy) has passed locally and any fixes were made

• All tests (pytest --runslow) have passed locally

This PR is related to the 1st PR: moving prints from Flight.py to flight_prints.py check box in #287

[Gui-FernandesBR]

Could we avoid the unecessary \n in the printxxxx methods?

I think simply replacing all the \n\n by \n would give a cleaner result, see an example here:

TestFlight.prints.all()

Result:

Initial Conditions

Position - x: 0.00 m | y: 0.00 m | z: 1400.00 m
Velocity - Vx: 0.00 m/s | Vy: 0.00 m/s | Vz: 0.00 m/s
Attitude - e0: 0.999 | e1: -0.044 | e2: -0.000 | e3: 0.000
Euler Angles - Spin φ : 0.00° | Nutation θ: -5.00° | Precession ψ: 0.00°
Angular Velocity - ω1: 0.00 rad/s | ω2: 0.00 rad/s| ω3: 0.00 rad/s

Surface Wind Conditions

Frontal Surface Wind Speed: 0.00 m/s
Lateral Surface Wind Speed: 0.00 m/s

Launch Rail Orientation

Launch Rail Inclination: 85.00°
Launch Rail Heading: 0.00°

Rail Departure State

Rail Departure Time: 0.363 s
Rail Departure Velocity: 25.799 m/s
Rail Departure Static Margin: 2.133 c
Rail Departure Angle of Attack: 0.000°
Rail Departure Thrust-Weight Ratio: 10.143
Rail Departure Reynolds Number: 2.009e+05

BurnOut State

BurnOut time: 3.900 s
Altitude at burnOut: 657.271 m (AGL)
Rocket velocity at burnOut: 279.521 m/s
Freestream velocity at burnOut: 279.521 m/s
Mach Number at burnOut: 0.842
Kinetic energy at burnOut: 6.345e+05 J

Apogee State

Apogee Altitude: 4699.958 m (ASL) | 3299.958 m (AGL)
Apogee Time: 25.834 s
Apogee Freestream Speed: 20.508 m/s

Parachute Events

Drogue Ejection Triggered at: 25.838 s
Drogue Parachute Inflated at: 27.338 s
Drogue Parachute Inflated with Freestream Speed of: 25.048 m/s
Drogue Parachute Inflated at Height of: 3289.077 m (AGL)
Main Ejection Triggered at: 158.105 s
Main Parachute Inflated at: 159.605 s
Main Parachute Inflated with Freestream Speed of: 17.967 m/s
Main Parachute Inflated at Height of: 773.002 m (AGL)

Impact Conditions

X Impact: 0.000 m
Y Impact: 681.833 m
Time of Impact: 297.728 s
Velocity at Impact: -5.459 m/s

Maximum Values

Maximum Speed: 285.840 m/s at 3.38 s
Maximum Mach Number: 0.860 Mach at 3.38 s
Maximum Reynolds Number: 2.138e+06 at 3.32 s
Maximum Dynamic Pressure: 4.151e+04 Pa at 3.34 s
Maximum Acceleration: 105.084 m/s² at 0.15 s
Maximum Gs: 10.716 g at 0.15 s
Maximum Upper Rail Button Normal Force: 0.257 N
Maximum Upper Rail Button Shear Force: 0.257 N
Maximum Lower Rail Button Normal Force: 0.257 N
Maximum Lower Rail Button Shear Force: 0.257 N

Numerical Integration Settings

Maximum Allowed Flight Time: 600.000000 s
Maximum Allowed Time Step: inf s
Minimum Allowed Time Step: 0.000000e+00 s
Relative Error Tolerance: 1e-06
Absolute Error Tolerance: [0.001, 0.001, 0.001, 0.001, 0.001, 0.001, 1e-06, 1e-06, 1e-06, 1e-06, 0.001, 0.001, 0.001]
Allow Event Overshoot: True
Terminate Simulation on Apogee: False
Number of Time Steps Used: 558
Number of Derivative Functions Evaluation: 1895
Average Function Evaluations per Time Step: 3.396057

[Gui-FernandesBR]

Good work here @MateusStano , really easy to review!

I made two comments, after addressing that, we will be able to approve/merge

[MateusStano]

Good work here @MateusStano , really easy to review!

I made two comments, after addressing that, we will be able to approve/merge

All done!

[Gui-FernandesBR]

Nice job here, congrats!

[Gui-FernandesBR]

@MateusStano feel free to merge this one