Plane: cope with the changed semantics if airspeed.use()

ArduPlane/ArduPlane.pde

@@ -1215,7 +1215,7 @@ static void handle_auto_mode(void)
             // allowed for level flight
             nav_roll_cd = constrain_int32(nav_roll_cd, -g.level_roll_limit*100UL, g.level_roll_limit*100UL);
         } else {
-            if (!airspeed.use()) {
+            if (!ahrs.airspeed_sensor_enabled()) {
                 // when not under airspeed control, don't allow
                 // down pitch in landing
                 nav_pitch_cd = constrain_int32(nav_pitch_cd, 0, nav_pitch_cd);

ArduPlane/Attitude.pde

@@ -558,7 +558,7 @@ static bool is_flying(void)
     bool gpsMovement = (gps.status() < AP_GPS::GPS_OK_FIX_2D ||
                         gps.ground_speed() >= 5);
     
-    bool airspeedMovement = !airspeed.use() || airspeed.get_airspeed() >= 5;
+    bool airspeedMovement = (!ahrs.airspeed_sensor_enabled()) || airspeed.get_airspeed() >= 5;
     
     // we're more than 5m from the home altitude
     bool inAir = relative_altitude_abs_cm() > 500;
@@ -614,7 +614,7 @@ static bool suppress_throttle(void)
         // if we have an airspeed sensor, then check it too, and
         // require 5m/s. This prevents throttle up due to spiky GPS
         // groundspeed with bad GPS reception
-        if (!airspeed.use() || airspeed.get_airspeed() >= 5) {
+        if ((!ahrs.airspeed_sensor_enabled()) || airspeed.get_airspeed() >= 5) {
             // we're moving at more than 5 m/s
             throttle_suppressed = false;
             return false;        
@@ -869,7 +869,7 @@ static void set_servos(void)
 
     if (auto_throttle_mode) {
         int16_t flapSpeedSource = 0;
-        if (airspeed.use()) {
+        if (ahrs.airspeed_sensor_enabled()) {
             flapSpeedSource = target_airspeed_cm * 0.01f;
         } else {
             flapSpeedSource = aparm.throttle_cruise;

ArduPlane/radio.pde

@@ -163,7 +163,7 @@ static void read_radio()
 
     if (g.throttle_nudge && channel_throttle->servo_out > 50) {
         float nudge = (channel_throttle->servo_out - 50) * 0.02f;
-        if (airspeed.use()) {
+        if (ahrs.airspeed_sensor_enabled()) {
             airspeed_nudge_cm = (aparm.airspeed_max * 100 - g.airspeed_cruise_cm) * nudge;
         } else {
             throttle_nudge = (aparm.throttle_max - aparm.throttle_cruise) * nudge;

ArduPlane/takeoff.pde

@@ -115,7 +115,7 @@ static void takeoff_calc_pitch(void)
         return;
     }
 
-    if (airspeed.use()) {
+    if (ahrs.airspeed_sensor_enabled()) {
         calc_nav_pitch();
         if (nav_pitch_cd < auto_state.takeoff_pitch_cd) {
             nav_pitch_cd = auto_state.takeoff_pitch_cd;