Move _TAScruise declaration to header

ArduPilot · Oct 31, 2023 · 0f5e800 · 0f5e800
1 parent bd9087e
commit 0f5e800
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Showing 2 changed files with 6 additions and 1 deletion.
diff --git a/libraries/AP_TECS/AP_TECS.cpp b/libraries/AP_TECS/AP_TECS.cpp
@@ -470,11 +470,13 @@ void AP_TECS::_update_speed_demand(void)
     // Constrain speed demand, taking into account the load factor
     _TAS_dem = constrain_float(_TAS_dem, _TASmin, _TASmax);
 
+    // Determine the true cruising airspeed (m/s)
+    _TAScruise = 0.01f * (float)aparm.airspeed_cruise_cm * _ahrs.get_EAS2TAS();
+
     // calculate velocity rate limits based on physical performance limits
     // provision to use a different rate limit if bad descent or underspeed condition exists
     // Use 50% of maximum energy rate on gain, 90% on dissipation to allow margin for total energy controller
     const float velRateMax = 0.5f * _STEdot_max / _TAS_state;
-    const float _TAScruise = 0.01f * (float)aparm.airspeed_cruise_cm * _ahrs.get_EAS2TAS();
     // Maximum permissible rate of deceleration value at max airspeed
     const float velRateNegMax = 0.9f * _STEdot_neg_max / _TASmax;
     // Maximum permissible rate of deceleration value at cruise speed

diff --git a/libraries/AP_TECS/AP_TECS.h b/libraries/AP_TECS/AP_TECS.h
@@ -266,6 +266,9 @@ class AP_TECS {
     float _TASmax;
     float _TASmin;
 
+    // True cruising airspeed (TRIM_ARSPD)
+    float _TAScruise;
+
     // Current true airspeed demand
     float _TAS_dem;