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Variables
cessna.proto File Reference

Variables

message Cessna
 
optional float cmd_elevators = 13
 Target elevators angle in rads. More...
 
optional float cmd_left_aileron = 9
 Target left aileron angle in rads. More...
 
optional float cmd_left_flap = 10
 Target left flap angle in rads. More...
 
optional float cmd_propeller_speed = 8
 Target RPM of the propeller. More...
 
optional float cmd_right_aileron = 11
 Target right aileron angle in rads. More...
 
optional float cmd_right_flap = 12
 Target right flap angle in rads. More...
 
optional float cmd_rudder = 14
 Target ruddle angle in rads. More...
 
optional float elevators = 6
 Current elevators angle in rads. More...
 
optional float left_aileron = 2
 Current left aileron angle in rads. More...
 
optional float left_flap = 3
 Current left flap angle in rads. More...
 
package gazebo msgs
 
optional float right_aileron = 4
 Current right aileron angle in rads. More...
 
optional float right_flap = 5
 Current right flap angle in rads. More...
 
optional float rudder = 7
 Current ruddle angle in rads. More...
 

Variable Documentation

message Cessna
Initial value:
{
optional float propeller_speed = 1
optional float cmd_elevators = 13

Target elevators angle in rads.

optional float cmd_left_aileron = 9

Target left aileron angle in rads.

optional float cmd_left_flap = 10

Target left flap angle in rads.

optional float cmd_propeller_speed = 8

Target RPM of the propeller.

optional float cmd_right_aileron = 11

Target right aileron angle in rads.

optional float cmd_right_flap = 12

Target right flap angle in rads.

optional float cmd_rudder = 14

Target ruddle angle in rads.

optional float elevators = 6

Current elevators angle in rads.

optional float left_aileron = 2

Current left aileron angle in rads.

optional float left_flap = 3

Current left flap angle in rads.

package gazebo msgs
optional float right_aileron = 4

Current right aileron angle in rads.

optional float right_flap = 5

Current right flap angle in rads.

optional float rudder = 7

Current ruddle angle in rads.