View source: R/get_pcoll_grid.R
get_pcoll_grid | R Documentation |
Calculates single transit collision risk at grid points (X, Y) inside the left-half of the rotor circle, for a given flight direction (upwind or downwind), and assuming no avoidance action. The origin of the (X, Y) coordinates is the rotor center
get_pcoll_grid( rotor_grids, direction, rotor_radius, blade_width, rotor_speed, blade_pitch, flight_type, n_blades, flight_speed, wing_span, body_lt )
rotor_grids |
A list object containing geometric attributes of the rotor
at equidistant points within its unit circle. This object should be
built via the function |
direction |
an integer, indicating the flight direction: 1 for upwind; -1 for downwind. |
rotor_radius |
Numeric value. The radius of the rotor (R), in metres. |
blade_width |
Numeric value, giving the maximum blade width, in metres. |
rotor_speed |
Numeric value. The operational rotation speed, in revolutions/min. |
blade_pitch |
Numeric value. The average blade pitch angle, the angle between the blade surface and the rotor plane (γ), in radians. |
flight_type |
A character string, either 'flapping' or 'gliding', indicating the species' characteristic flight type. |
n_blades |
An integer, the number of blades in rotor (b). |
flight_speed |
Numeric value. The bird flying speed (v), in metres/sec. |
wing_span |
Numeric value. The wingspan of the bird (W), in metres. |
body_lt |
Numeric value. The length of the bird (L), in metres. |
Methodology and assumptions underpinning get_pcoll_grid
are
described in section "Extended Approach Taking Account Of Flight Heights" of
Band (2012). Note that collision risk calculations are based on equation (3)
in "Stage C" section, but using (X, Y) coordinates to reference transit
points instead of the equivalent (r, phi) coordinates.
a matrix. The probability of collisions at different flight height bands
generate_rotor_grids
rotor_grids <- generate_rotor_grids(yinc = 0.05, xinc = 0.05, chord_prof_5MW) get_pcoll_grid( rotor_grids = rotor_grids, direction = 1, rotor_radius = 120, blade_width = 5, rotor_speed = 15, blade_pitch = 15, flight_type = "flapping", n_blades = 3, flight_speed = 13.1, wing_span = 1.01, body_lt = 0.85)
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