Changes between Initial Version and Version 1 of doc/app/virtual_flight_parameters

Timestamp:

Jul 4, 2016 4:22:27 PM (9 years ago)

Author:

suehring

Comment:

--

doc/app/virtual_flight_parameters

@@ +1 @@
+
+= Virtual flight parameters =
+
+\\\\
+NAMELIST group name: [=#flight_par '''flight_par''']\\
+----
+
+
+[=#mode '''Mode:]\\
+||='''Parameter Name'''  =||='''[../fortrantypes FORTRAN]\\[../fortrantypes Type]'''  =||='''Default\\Value'''  =||='''Explanation'''  =||
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#flight_angle '''flight_angle''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100*45.0
+}}}
+{{{#!td
+Horizontal flight angle in degrees describing the flight direction. For example, if [#flight_angle flight_angle] = 0.0 (180.0), the aircraft moves parallel to the x-axis in positive (negative) x-direction, respectively. If [#flight_angle flight_angle] = 90.0 (270.0), the aircraft moves parallel to the y-axis in positive (negative) y-direction, respectively. Please note, the parameters has only an effect if the respective [#leg leg] is in 'cyclic'-mode, else the flight direction is determined by [#x_start x_start], [#x_end x_end], [#y_start y_start] and [#y_end y_end]
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#flight_end '''flight_end''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+9999999.9
+}}}
+{{{#!td
+End time of virtual flight measurement.
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#flight_start '''flight_start''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+0.0
+}}}
+{{{#!td
+Start time of virtual flight measurement.
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#leg '''leg''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+C (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100*'cyclic'
+}}}
+{{{#!td
+Flight mode, either 'cyclic' or 'return'. In case of 'cyclic', the sensor keep moving further if the end-position (see [#x_end x_end] and [#y_end y_end]) is reached, i.e. the sensor moves cyclically through the model domain. Instead, in case of 'return', the sensor turns around at the end-position and flies back, where it turns around again at the start-position. This case, the sensor only moves between start- and end-position.   
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#level '''level''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100*100.0
+}}}
+{{{#!td
+Flight level in meter. Please note, level is given with respect to sea level, not with respect to the underlying terrain. 
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#max_elev_change '''max_elev_change''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100*0.0
+}}}
+{{{#!td
+Maximum possible elevation change in case [#rate_of_climb rate_of_climb] is not equal to zero. If the maximum elevation change is reached, the virtual aircraft start descending until the original start level is reached again. For longer flights, the sensor moves vertically between [#level level] and [#level level] + [#max_elev_change max_elev_change].
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#rate_of_climb '''rate_of_climb''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100*0.0
+}}}
+{{{#!td
+Vertical speed of the aircraft in meter per second.
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#speed_agl '''speed_agl''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100*25.0
+}}}
+{{{#!td
+Horizontal speed of the aircraft above ground level in meter per second.
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#x_end '''x_end''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100* \\
+999999999.0
+}}}
+{{{#!td
+End-position of the flight leg along x in meter. Please note, in case [#leg leg]='cyclic', the aircraft moves beyond the x-end-position until it reaches the lateral boundary of the model domain, where cyclic boundary conditions are assumed. 
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#x_start '''x_start''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100* \\
+999999999.0
+}}}
+{{{#!td
+Start-position of the flight leg along x in meter. 
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#y_end '''y_end''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100* \\
+999999999.0
+}}}
+{{{#!td
+Start-position of the flight leg along y in meter. 
+}}}
+|----------------
+{{{#!td style="vertical-align:top;width: 150px"
+[=#y_end '''y_end''']
+}}}
+{{{#!td style="vertical-align:top;width: 50px"
+R (100)
+}}}
+{{{#!td style="vertical-align:top;width: 75px"
+100* \\
+999999999.0
+}}}
+{{{#!td
+End-position of the flight leg along y in meter. 
+}}}