Mirror/ardupilot
5
0
Fork 0
mirror of https://github.com/ArduPilot/ardupilot synced 2025-01-03 06:28:27 -04:00
Code Issues Packages Projects Releases Wiki Activity

Copter: Fix typo

Browse Source 
Signed-off-by: Patrick José Pereira <patrickelectric@gmail.com>
This commit is contained in:
Patrick José Pereira 2019-03-25 20:57:55 -03:00 committed by Randy Mackay
parent 55047324ac
commit 33764d6c3b
13 changed files with 14 additions and 14 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

2
ArduCopter/APM_Config_mavlink_hil.h
View File

@ -4,7 +4,7 @@
// 1. HIL_MODE_SENSORS: full sensor simulation
#define HIL_MODE HIL_MODE_SENSORS
// HIL_PORT SELCTION
// HIL_PORT SELECTION
//
// PORT 1
// If you would like to run telemetry communications for a groundstation

2
ArduCopter/Copter.h
View File

@ -261,7 +261,7 @@ private:
SITL::SITL sitl;
#endif
// Arming/Disarming mangement class
// Arming/Disarming management class
AP_Arming_Copter arming;
// Optical flow sensor

2
ArduCopter/GCS_Mavlink.cpp
View File

@ -1298,7 +1298,7 @@ bool GCS_MAVLINK_Copter::set_mode(const uint8_t mode)
float GCS_MAVLINK_Copter::vfr_hud_alt() const
{
if (copter.g2.dev_options.get() & DevOptionVFR_HUDRelativeAlt) {
// compatability option for older mavlink-aware devices that
// compatibility option for older mavlink-aware devices that
// assume Copter returns a relative altitude in VFR_HUD.alt
return copter.current_loc.alt / 100.0f;
}

2
ArduCopter/Parameters.cpp
View File

@ -1316,7 +1316,7 @@ void Copter::convert_tradheli_parameters(void)
{ Parameters::k_param_motors, 19, AP_PARAM_INT8, "H_SW_COL_DIR" },
};
// convert single heli paramters without scaling
// convert single heli parameters without scaling
uint8_t table_size = ARRAY_SIZE(singleheli_conversion_info);
for (uint8_t i=0; i<table_size; i++) {
AP_Param::convert_old_parameter(&singleheli_conversion_info[i], 1.0f);

2
ArduCopter/Parameters.h
View File

@ -259,7 +259,7 @@ public:
k_param_camera_mount2, // deprecated
//
// Batery monitoring parameters
// Battery monitoring parameters
//
k_param_battery_volt_pin = 168, // deprecated - can be deleted
k_param_battery_curr_pin, // 169 deprecated - can be deleted

4
ArduCopter/RC_Channel.cpp
View File

@ -2,7 +2,7 @@
#include "RC_Channel.h"
// defining these two macros and including the RC_Channels_VarInfo header defines the parmaeter information common to all vehicle types
// defining these two macros and including the RC_Channels_VarInfo header defines the parameter information common to all vehicle types
#define RC_CHANNELS_SUBCLASS RC_Channels_Copter
#define RC_CHANNEL_SUBCLASS RC_Channel_Copter
@ -136,7 +136,7 @@ void RC_Channel_Copter::do_aux_function_change_mode(const control_mode_t mode,
}
}
// do_aux_function - implement the function invoked by auxillary switches
// do_aux_function - implement the function invoked by auxiliary switches
void RC_Channel_Copter::do_aux_function(const aux_func_t ch_option, const aux_switch_pos_t ch_flag)
{
switch(ch_option) {

2
ArduCopter/config.h
View File

@ -159,7 +159,7 @@
// Radio failsafe
#ifndef FS_RADIO_TIMEOUT_MS
#define FS_RADIO_TIMEOUT_MS 500 // RC Radio Failsafe triggers after 500 miliseconds with No RC Input
#define FS_RADIO_TIMEOUT_MS 500 // RC Radio Failsafe triggers after 500 milliseconds with No RC Input
#endif
// missing terrain data failsafe

2
ArduCopter/ekf_check.cpp
View File

@ -16,7 +16,7 @@
#endif
////////////////////////////////////////////////////////////////////////////////
// EKF_check strucutre
// EKF_check structure
////////////////////////////////////////////////////////////////////////////////
static struct {
uint8_t fail_count; // number of iterations ekf or dcm have been out of tolerances

2
ArduCopter/mode.cpp
View File

@ -479,7 +479,7 @@ void Copter::Mode::land_run_horizontal_control()
// convert pilot input to lean angles
get_pilot_desired_lean_angles(target_roll, target_pitch, loiter_nav->get_angle_max_cd(), attitude_control->get_althold_lean_angle_max());
// record if pilot has overriden roll or pitch
// record if pilot has overridden roll or pitch
if (!is_zero(target_roll) || !is_zero(target_pitch)) {
if (!ap.land_repo_active) {
copter.Log_Write_Event(DATA_LAND_REPO_ACTIVE);

2
ArduCopter/mode_poshold.cpp
View File

@ -499,7 +499,7 @@ void Copter::ModePosHold::run()
if (!is_zero(target_pitch)) {
// init transition to pilot override
poshold_pitch_controller_to_pilot_override();
// if roll not overriden switch roll-mode to brake (but be ready to go back to loiter any time)
// if roll not overridden switch roll-mode to brake (but be ready to go back to loiter any time)
if (is_zero(target_roll)) {
poshold.roll_mode = POSHOLD_BRAKE_READY_TO_LOITER;
poshold.brake_roll = 0;

2
ArduCopter/mode_rtl.cpp
View File

@ -285,7 +285,7 @@ void Copter::ModeRTL::descent_run()
// convert pilot input to lean angles
get_pilot_desired_lean_angles(target_roll, target_pitch, loiter_nav->get_angle_max_cd(), attitude_control->get_althold_lean_angle_max());
// record if pilot has overriden roll or pitch
// record if pilot has overridden roll or pitch
if (!is_zero(target_roll) || !is_zero(target_pitch)) {
if (!ap.land_repo_active) {
copter.Log_Write_Event(DATA_LAND_REPO_ACTIVE);

2
ArduCopter/motor_test.cpp
View File

@ -82,7 +82,7 @@ void Copter::motor_test_output()
// sanity check throttle values
if (pwm >= MOTOR_TEST_PWM_MIN && pwm <= MOTOR_TEST_PWM_MAX ) {
// turn on motor to specified pwm vlaue
// turn on motor to specified pwm value
motors->output_test_seq(motor_test_seq, pwm);
} else {
motor_test_stop();

2
ArduCopter/motors.cpp
View File

@ -223,7 +223,7 @@ bool Copter::init_arm_motors(const AP_Arming::Method method, const bool do_armin
// log flight mode in case it was changed while vehicle was disarmed
logger.Write_Mode(control_mode, control_mode_reason);
// reenable failsafe
// re-enable failsafe
failsafe_enable();
// perf monitor ignores delay due to arming