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clang-tidy modernize-redundant-void-arg
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@@ -171,7 +171,7 @@ void TECS::_update_speed(float airspeed_demand, float indicated_airspeed,
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_update_speed_last_usec = now;
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}
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void TECS::_update_speed_demand(void)
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void TECS::_update_speed_demand()
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{
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// Set the airspeed demand to the minimum value if an underspeed condition exists
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// or a bad descent condition exists
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@@ -276,7 +276,7 @@ void TECS::_update_height_demand(float demand, float state)
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//warnx("_hgt_rate_dem: %.4f, _hgt_dem_adj %.4f", _hgt_rate_dem, _hgt_dem_adj);
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}
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void TECS::_detect_underspeed(void)
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void TECS::_detect_underspeed()
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{
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if (!_detect_underspeed_enabled) {
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_underspeed = false;
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@@ -291,7 +291,7 @@ void TECS::_detect_underspeed(void)
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}
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}
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void TECS::_update_energies(void)
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void TECS::_update_energies()
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{
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// Calculate specific energy demands
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_SPE_dem = _hgt_dem_adj * CONSTANTS_ONE_G;
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@@ -393,7 +393,7 @@ void TECS::_update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotM
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}
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}
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void TECS::_detect_bad_descent(void)
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void TECS::_detect_bad_descent()
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{
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// Detect a demanded airspeed too high for the aircraft to achieve. This will be
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// evident by the the following conditions:
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@@ -421,7 +421,7 @@ void TECS::_detect_bad_descent(void)
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_badDescent = false;
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}
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void TECS::_update_pitch(void)
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void TECS::_update_pitch()
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{
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// Calculate Speed/Height Control Weighting
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// This is used to determine how the pitch control prioritises speed and height control
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@@ -544,7 +544,7 @@ void TECS::_initialise_states(float pitch, float throttle_cruise, float baro_alt
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_states_initalized = true;
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}
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void TECS::_update_STE_rate_lim(void)
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void TECS::_update_STE_rate_lim()
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{
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// Calculate Specific Total Energy Rate Limits
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// This is a trivial calculation at the moment but will get bigger once we start adding altitude effects
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@@ -24,7 +24,7 @@ extern "C" __EXPORT int rc_tests_main(int argc, char *argv[]);
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class RCTest : public UnitTest
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{
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public:
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virtual bool run_tests(void);
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virtual bool run_tests();
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private:
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bool dsmTest(const char *filepath, unsigned expected_chancount, unsigned expected_dropcount, unsigned chan0);
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@@ -35,7 +35,7 @@ private:
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bool sumdTest();
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};
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bool RCTest::run_tests(void)
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bool RCTest::run_tests()
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{
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ut_run_test(dsmTest10Ch);
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ut_run_test(dsmTest12Ch);
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@@ -131,7 +131,7 @@ bool RCTest::dsmTest(const char *filepath, unsigned expected_chancount, unsigned
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return true;
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}
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bool RCTest::sbus2Test(void)
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bool RCTest::sbus2Test()
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{
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const char *filepath = TEST_DATA_PATH "sbus2_r7008SB.txt";
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@@ -212,7 +212,7 @@ bool RCTest::sbus2Test(void)
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return true;
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}
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bool RCTest::st24Test(void)
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bool RCTest::st24Test()
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{
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const char *filepath = TEST_DATA_PATH "st24_data.txt";
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@@ -273,7 +273,7 @@ bool RCTest::st24Test(void)
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return true;
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}
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bool RCTest::sumdTest(void)
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bool RCTest::sumdTest()
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{
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const char *filepath = TEST_DATA_PATH "sumd_data.txt";
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