Struct Log 

pub struct Log {
    pub file: &'static str,
    pub header_lines: usize,
    pub time_column: usize,
    pub height_column: usize,
    pub meters_per_unit: f64,
    pub until_s: Option<f64>,
    pub altimeter: Altimeter,
    pub pressure: Option<(usize, f64)>,
    pub gnss: Option<Gnss>,
}

Where a flight’s altitude log is and how to read it.

Fields

file: &'static str

The CSV file, under refs/rocketpy/data/rockets/.

header_lines: usize

Header lines before the first row.

time_column: usize

The column of time, s (zero-based).

height_column: usize

The column of height above the pad (zero-based), used as recorded.

meters_per_unit: f64

Meters per unit of the height column.

until_s: Option<f64>

Rows after this time are not read, s: where the log stops recording the rocket’s height, at an ejection charge’s pressure transient past apogee or a corrupted end. The flight’s RealFlight::note says which.

altimeter: Altimeter

What measured the height, and so what of hpr’s flight it is compared with.

pressure: Option<(usize, f64)>

The column of the pressure the height was read from, and pascals per unit, where the log keeps it: the report gives how far the height column is from the standard atmosphere’s reading of it.

gnss: Option<Gnss>

The flight’s satellite (GNSS) altitude, where it logged one: a geometric height to hold the barometric reading against.

Trait Implementations

impl Clone for Log

fn clone(&self) -> Log

Returns a duplicate of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Copy for Log

impl Debug for Log

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.

impl PartialEq for Log

fn eq(&self, other: &Log) -> bool

Tests for self and other values to be equal, and is used by ==.

fn ne(&self, other: &Rhs) -> bool

Tests for !=. The default implementation is almost always sufficient, and should not be overridden without very good reason.

impl StructuralPartialEq for Log