diff options
-rw-r--r-- | Documentation/rc_mode_switch.odg | bin | 20160 -> 20920 bytes | |||
-rw-r--r-- | Documentation/rc_mode_switch.pdf | bin | 39286 -> 27305 bytes | |||
-rw-r--r-- | mavlink/include/mavlink/v1.0/autoquad/autoquad.h | 4 | ||||
-rw-r--r-- | src/modules/fixedwing_backside/fixedwing.cpp | 2 |
4 files changed, 3 insertions, 3 deletions
diff --git a/Documentation/rc_mode_switch.odg b/Documentation/rc_mode_switch.odg Binary files differindex 5c4b617e6..3ed379d08 100644 --- a/Documentation/rc_mode_switch.odg +++ b/Documentation/rc_mode_switch.odg diff --git a/Documentation/rc_mode_switch.pdf b/Documentation/rc_mode_switch.pdf Binary files differindex 3254d6140..70e7cb246 100644 --- a/Documentation/rc_mode_switch.pdf +++ b/Documentation/rc_mode_switch.pdf diff --git a/mavlink/include/mavlink/v1.0/autoquad/autoquad.h b/mavlink/include/mavlink/v1.0/autoquad/autoquad.h index bd3fc66e7..05794725a 100644 --- a/mavlink/include/mavlink/v1.0/autoquad/autoquad.h +++ b/mavlink/include/mavlink/v1.0/autoquad/autoquad.h @@ -40,8 +40,8 @@ enum AUTOQUAD_NAV_STATUS AQ_NAV_STATUS_INIT=0, /* System is initializing | */ AQ_NAV_STATUS_STANDBY=1, /* System is standing by, not active | */ AQ_NAV_STATUS_MANUAL=2, /* Stabilized, under full manual control | */ - AQ_NAV_STATUS_ALTCTRL=4, /* Altitude hold engaged | */ - AQ_NAV_STATUS_POSCTRL=8, /* Position hold engaged | */ + AQ_NAV_STATUS_ALTCTRL=4, /* Altitude control engaged | */ + AQ_NAV_STATUS_POSCTRL=8, /* Position control engaged | */ AQ_NAV_STATUS_DVH=16, /* Dynamic Velocity Hold is active | */ AQ_NAV_STATUS_MISSION=32, /* Autonomous mission execution mode | */ AQ_NAV_STATUS_CEILING_REACHED=67108864, /* Craft is at ceiling altitude | */ diff --git a/src/modules/fixedwing_backside/fixedwing.cpp b/src/modules/fixedwing_backside/fixedwing.cpp index dc82ee475..596e286a4 100644 --- a/src/modules/fixedwing_backside/fixedwing.cpp +++ b/src/modules/fixedwing_backside/fixedwing.cpp @@ -230,7 +230,7 @@ void BlockMultiModeBacksideAutopilot::update() _actuators.control[CH_THR] = _manual.throttle; } else if (_status.main_state == MAIN_STATE_ALTCTRL || - _status.main_state == MAIN_STATE_POSCTRL /* TODO, implement easy */) { + _status.main_state == MAIN_STATE_POSCTRL /* TODO, implement pos control */) { // calculate velocity, XXX should be airspeed, but using ground speed for now // for the purpose of control we will limit the velocity feedback between |