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APM: rename airspeed_cruise to airspeed_cruise_cm to make the units clearer 

it is in cm/s, not m/s
This commit is contained in:
Andrew Tridgell 2012-07-19 10:52:08 +10:00
parent 1cf5057c61
commit d6e370886f
7 changed files with 10 additions and 10 deletions
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2
ArduPlane/ArduPlane.pde
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@ -995,7 +995,7 @@ static void update_current_flight_mode(void)
if(nav_pitch < (long)takeoff_pitch)
nav_pitch = (long)takeoff_pitch;
} else {
nav_pitch = (long)((float)g_gps->ground_speed / (float)g.airspeed_cruise * (float)takeoff_pitch * 0.5);
nav_pitch = (long)((float)g_gps->ground_speed / (float)g.airspeed_cruise_cm * (float)takeoff_pitch * 0.5);
nav_pitch = constrain(nav_pitch, 500l, (long)takeoff_pitch);
}

4
ArduPlane/Attitude.pde
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@ -210,7 +210,7 @@ static void calc_nav_roll()
if(airspeed.use()) {
speed = airspeed.get_airspeed();
} else {
speed = g.airspeed_cruise*0.01;
speed = g.airspeed_cruise_cm*0.01;
// Floor the speed so that the user can't enter a bad value
if(speed < 6) {
@ -384,7 +384,7 @@ static void set_servos(void)
if (control_mode == FLY_BY_WIRE_B) {
flapSpeedSource = ((float)target_airspeed)/100;
} else if (airspeed.use()) {
flapSpeedSource = g.airspeed_cruise/100;
flapSpeedSource = g.airspeed_cruise_cm/100;
} else {
flapSpeedSource = g.throttle_cruise;
}

6
ArduPlane/Parameters.h
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@ -116,7 +116,7 @@ public:
k_param_roll_limit,
k_param_pitch_limit_max,
k_param_pitch_limit_min,
k_param_airspeed_cruise,
k_param_airspeed_cruise_cm,
k_param_RTL_altitude,
k_param_inverted_flight_ch,
k_param_min_gndspeed,
@ -336,7 +336,7 @@ public:
AP_Int16 log_last_filenumber; // *** Deprecated - remove with next eeprom number change
AP_Int8 reset_switch_chan;
AP_Int8 manual_level;
AP_Int16 airspeed_cruise;
AP_Int16 airspeed_cruise_cm;
AP_Int16 min_gndspeed;
AP_Int16 pitch_trim;
AP_Int16 RTL_altitude;
@ -455,7 +455,7 @@ public:
log_last_filenumber (0),
reset_switch_chan (0),
manual_level (MANUAL_LEVEL),
airspeed_cruise (AIRSPEED_CRUISE_CM),
airspeed_cruise_cm (AIRSPEED_CRUISE_CM),
min_gndspeed (MIN_GNDSPEED_CM),
pitch_trim (0),
RTL_altitude (ALT_HOLD_HOME_CM),

2
ArduPlane/Parameters.pde
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@ -383,7 +383,7 @@ static const AP_Param::Info var_info[] PROGMEM = {
// @Description: Airspeed in cm/s to aim for when airspeed is enabled in auto mode
// @Units: cm/s
// @User: User
GSCALAR(airspeed_cruise, "TRIM_ARSPD_CM"),
GSCALAR(airspeed_cruise_cm, "TRIM_ARSPD_CM"),
// @Param: MIN_GNDSPD_CM
// @DisplayName: Minimum ground speed

2
ArduPlane/commands_logic.pde
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@ -523,7 +523,7 @@ static void do_change_speed()
{
case 0: // Airspeed
if(next_nonnav_command.alt > 0)
g.airspeed_cruise.set(next_nonnav_command.alt * 100);
g.airspeed_cruise_cm.set(next_nonnav_command.alt * 100);
break;
case 1: // Ground speed
g.min_gndspeed.set(next_nonnav_command.alt * 100);

2
ArduPlane/navigation.pde
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@ -67,7 +67,7 @@ static void calc_airspeed_errors()
float aspeed_cm = airspeed.get_airspeed_cm();
// Normal airspeed target
target_airspeed = g.airspeed_cruise;
target_airspeed = g.airspeed_cruise_cm;
// FBW_B airspeed target
if (control_mode == FLY_BY_WIRE_B) {

2
ArduPlane/radio.pde
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@ -90,7 +90,7 @@ static void read_radio()
if (g.channel_throttle.servo_out > 50) {
if (airspeed.use()) {
airspeed_nudge = (g.flybywire_airspeed_max * 100 - g.airspeed_cruise) * ((g.channel_throttle.norm_input()-0.5) / 0.5);
airspeed_nudge = (g.flybywire_airspeed_max * 100 - g.airspeed_cruise_cm) * ((g.channel_throttle.norm_input()-0.5) / 0.5);
} else {
throttle_nudge = (g.throttle_max - g.throttle_cruise) * ((g.channel_throttle.norm_input()-0.5) / 0.5);
}