Plane: fixed misspellings of 'transition'

ArduPlane/mode_qacro.cpp

@@ -6,7 +6,7 @@
 bool ModeQAcro::_enter()
 {
     quadplane.throttle_wait = false;
-    quadplane.transition->force_transistion_complete();
+    quadplane.transition->force_transition_complete();
     attitude_control->relax_attitude_controllers();
     return true;
 }

ArduPlane/quadplane.cpp

@@ -756,7 +756,7 @@ bool QuadPlane::setup(void)
     // init wp_nav variables after detaults are setup
     wp_nav->wp_and_spline_init();
 
-    transition->force_transistion_complete();
+    transition->force_transition_complete();
 
     // param count will have changed
     AP_Param::invalidate_count();
@@ -1747,7 +1747,7 @@ void QuadPlane::update(void)
                 set_desired_spool_state(AP_Motors::DesiredSpoolState::SHUT_DOWN);
                 motors->output();
             }
-            transition->force_transistion_complete();
+            transition->force_transition_complete();
             assisted_flight = false;
         } else {
             transition->update();
@@ -3292,7 +3292,7 @@ void QuadPlane::Log_Write_QControl_Tuning()
         climb_rate          : int16_t(inertial_nav.get_velocity_z_up_cms()),
         throttle_mix        : attitude_control->get_throttle_mix(),
         speed_scaler        : tailsitter.log_spd_scaler,
-        transition_state    : transition->get_log_transision_state(),
+        transition_state    : transition->get_log_transition_state(),
         assist              : assisted_flight,
     };
     plane.logger.WriteBlock(&pkt, sizeof(pkt));
@@ -4085,7 +4085,7 @@ void SLT_Transition::set_last_fw_pitch()
     last_fw_nav_pitch_cd = plane.nav_pitch_cd;
 }
 
-void SLT_Transition::force_transistion_complete() {
+void SLT_Transition::force_transition_complete() {
     transition_state = TRANSITION_DONE; 
     in_forced_transition = false;
     transition_start_ms = 0;

ArduPlane/tailsitter.cpp

@@ -832,7 +832,7 @@ void Tailsitter_Transition::VTOL_update()
     if (transition_state == TRANSITION_ANGLE_WAIT_VTOL) {
         float aspeed;
         bool have_airspeed = quadplane.ahrs.airspeed_estimate(aspeed);
-        // provide assistance in forward flight portion of tailsitter transistion
+        // provide assistance in forward flight portion of tailsitter transition
         quadplane.assisted_flight = quadplane.should_assist(aspeed, have_airspeed);
         if (!quadplane.tailsitter.transition_vtol_complete()) {
             return;
@@ -937,7 +937,7 @@ void Tailsitter_Transition::restart()
 }
 
 // force state to FW and setup for the transition back to VTOL
-void Tailsitter_Transition::force_transistion_complete()
+void Tailsitter_Transition::force_transition_complete()
 {
     transition_state = TRANSITION_DONE;
     vtol_transition_start_ms = AP_HAL::millis();

ArduPlane/tailsitter.h

@@ -54,7 +54,7 @@ public:
     // check if we have completed transition to vtol
     bool transition_vtol_complete(void) const;
 
-    // return true if transistion to VTOL flight
+    // return true if transition to VTOL flight
     bool in_vtol_transition(uint32_t now = 0) const;
 
     // account for control surface speed scaling in VTOL modes
@@ -144,14 +144,14 @@ public:
 
     void VTOL_update() override;
 
-    void force_transistion_complete() override;
+    void force_transition_complete() override;
 
     bool complete() const override { return transition_state == TRANSITION_DONE; }
 
     // setup for the transition back to fixed wing
     void restart() override;
 
-    uint8_t get_log_transision_state() const override { return static_cast<uint8_t>(transition_state); }
+    uint8_t get_log_transition_state() const override { return static_cast<uint8_t>(transition_state); }
 
     bool active() const override { return transition_state != TRANSITION_DONE; }
 

ArduPlane/tiltrotor.cpp

@@ -74,7 +74,7 @@ const AP_Param::GroupInfo Tiltrotor::var_info[] = {
 
     // @Param: WING_FLAP
     // @DisplayName: Tiltrotor tilt angle that will be used as flap
-    // @Description: For use on tilt wings, the wing will tilt up to this angle for flap, transistion will be complete when the wing reaches this angle from the forward fight position, 0 disables
+    // @Description: For use on tilt wings, the wing will tilt up to this angle for flap, transition will be complete when the wing reaches this angle from the forward fight position, 0 disables
     // @Units: deg
     // @Increment: 1
     // @Range: 0 15

ArduPlane/transition.h

@@ -28,13 +28,13 @@ public:
 
     virtual void VTOL_update() = 0;
 
-    virtual void force_transistion_complete() = 0;
+    virtual void force_transition_complete() = 0;
 
     virtual bool complete() const = 0;
 
     virtual void restart() = 0;
 
-    virtual uint8_t get_log_transision_state() const = 0;
+    virtual uint8_t get_log_transition_state() const = 0;
 
     virtual bool active() const = 0;
 
@@ -75,13 +75,13 @@ public:
 
     void VTOL_update() override;
 
-    void force_transistion_complete() override;
+    void force_transition_complete() override;
 
     bool complete() const override { return transition_state == TRANSITION_DONE; }
 
     void restart() override { transition_state = TRANSITION_AIRSPEED_WAIT; }
 
-    uint8_t get_log_transision_state() const override { return static_cast<uint8_t>(transition_state); }
+    uint8_t get_log_transition_state() const override { return static_cast<uint8_t>(transition_state); }
 
     bool active() const override;