3 releases
0.1.2 | Feb 17, 2023 |
---|---|
0.1.1 | Feb 3, 2023 |
0.1.0 | Jan 20, 2023 |
#398 in Science
60KB
1K
SLoC
donnager.rs
A library of functions for blazingly fast astrodynamic calculations.
Until the rains fall on Olympus Mons.
Note: Under active development, updating structure frequently.
Stable release TBD
Installation
cargo install donnager
or, alternatively, in your project's cargo.toml
file:
[dependencies]
donnager = "0.1.2"
Modules
cosmos
dynamics
propulsion
Example Usage
use donnager::constants as cst;
use donnager::cosmos as cosm;
use donnager::propulsion as prop;
use donnager::dynamics as dynam;
use nalgebra as na;
use na::Vector3;
// Config
let earth: cosm::gravity::Body = cosm::gravity::Body {
name: "Earth".to_string(),
grav_param: cst::EARTH_GRAV_PARAM,
eq_radius: cst::EARTH_RADIUS_EQUATOR,
rotation_rate: cst::EARTH_ROT_RATE,
eccentricity: cst::EARTH_ECC
};
let launch_site: cosm::space::SurfacePoint = cosm::space::SurfacePoint {
name: "Cape Canaveral Launch Site".to_string(),
body: earth.clone(),
pos_lla: Vector3::new(28.396837, -80.605659, 0.0)
};
let payload_eng: prop::engine::Engine = prop::engine::Engine{
name: "Payload_Engine".to_string(),
engine_type: prop::engine::EngineType::Electric,
isp: 500.0
};
let payload: dynam::vehicle::Vehicle = dynam::vehicle::Vehicle {
name: "Satellite_1".to_string(),
mass: 5.0,
engine: payload_eng
};
let stage1_eng: prop::engine::Engine = prop::engine::Engine{
name: "Hydrolox Dual Flow".to_string(),
engine_type: prop::engine::EngineType::Chemical,
isp: 300.0
};
let stage_1: dynam::vehicle::Vehicle = dynam::vehicle::Vehicle {
name: "Stage_1".to_string(),
mass: 250.0,
engine: stage1_eng
};
let launch_vehicle: dynam::vehicle::Multistage = dynam::vehicle::Multistage{
name: "Launcher_7".to_string(),
stages: [stage_1, payload].to_vec()
};
// Inputs
let altitude: f64 = 408000.0; // LEO
// Calculation
let delta_v: f64 = launch_site.calc_delta_v(altitude);
let mass_fuel: Vec<f64> = launch_vehicle.calc_mass_fuel(delta_v, launch_site);
// Results
println!("\n{:.4} kg of fuel to get {} kg to {} m alt", mass_fuel[0], launch_vehicle.stages[1].mass, altitude);
Ad astra, plus ultra
Dependencies
~9MB
~162K SLoC