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style: clang-format new rules applied to the code base

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Mateusz Pusz
2023-05-26 14:20:00 +02:00
parent 561fbf7c93
commit 52bbd00ab4
20 changed files with 78 additions and 60 deletions
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example/CMakeLists.txt
+9 -1
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@@ -58,7 +58,15 @@ add_example(
strong_angular_quantities mp-units::core-fmt mp-units::core-io mp-units::si mp-units::isq_angle mp-units::utility
)
add_example(total_energy mp-units::core-io mp-units::si mp-units::natural mp-units::utility)
add_example(unmanned_aerial_vehicle mp-units::core-fmt mp-units::core-io mp-units::si mp-units::international mp-units::utility example_utils)
add_example(
unmanned_aerial_vehicle
mp-units::core-fmt
mp-units::core-io
mp-units::si
mp-units::international
mp-units::utility
example_utils
)
add_subdirectory(glide_computer)
add_subdirectory(kalman_filter)
example/currency.cpp
+1 -1
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@@ -88,4 +88,4 @@ int main()
std::cout << price_usd.absolute() << " -> " << price_euro.absolute() << "\n";
// std::cout << price_usd.absolute() + price_euro.absolute() << "\n"; // does not compile
}
}
example/foot_pound_second.cpp
+1 -1
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@@ -106,7 +106,7 @@ int main()
.speed{28.3 * kt},
.mass{42'245 * imperial::long_ton},
.mainGuns{14 * in},
.shellMass{1'590 * lb},
.shellMass{1590 * lb},
.shellSpeed{2483. * (ft / s)},
.power{110'000 * hp}};
example/glide_computer_example.cpp
+5 -4
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@@ -84,10 +84,11 @@ void print(const R& gliders)
std::cout << "- Polar:\n";
for (const auto& p : g.polar) {
const auto ratio = value_cast<one>(glide_ratio(g.polar[0]));
std::cout << UNITS_STD_FMT::format(" * {:%.4Q %q} @ {:%.1Q %q} -> {:%.1Q %q} ({:%.1Q %q})\n", p.climb, p.v, ratio,
// TODO is it possible to make ADL work below (we need another set of trig functions
// for strong angle in a different namespace)
value_cast<si::degree>(isq::asin(1 / ratio)));
std::cout << UNITS_STD_FMT::format(" * {:%.4Q %q} @ {:%.1Q %q} -> {:%.1Q %q} ({:%.1Q %q})\n", p.climb, p.v,
ratio,
// TODO is it possible to make ADL work below (we need another set of trig
// functions for strong angle in a different namespace)
value_cast<si::degree>(isq::asin(1 / ratio)));
}
std::cout << "\n";
}
example/kalman_filter/kalman_filter-example_1.cpp
+2 -2
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@@ -50,8 +50,8 @@ int main()
using state = kalman::state<quantity<isq::mass[g]>>;
const state initial = {1 * kg};
const std::array measurements = {1'030 * g, 989 * g, 1'017 * g, 1'009 * g, 1'013 * g,
979 * g, 1'008 * g, 1'042 * g, 1'012 * g, 1'011 * g};
const std::array measurements = {1'030 * g, 989 * g, 1'017 * g, 1'009 * g, 1'013 * g,
979 * g, 1'008 * g, 1'042 * g, 1'012 * g, 1'011 * g};
print_header(initial);
state next = initial;
example/kalman_filter/kalman_filter-example_2.cpp
+3 -2
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@@ -54,8 +54,9 @@ int main()
const auto interval = isq::duration(5 * s);
const state initial = {30 * km, 40 * (m / s)};
const quantity<isq::position_vector[m], int> measurements[] = {30'110 * m, 30'265 * m, 30'740 * m, 30'750 * m, 31'135 * m,
31'015 * m, 31'180 * m, 31'610 * m, 31'960 * m, 31'865 * m};
const quantity<isq::position_vector[m], int> measurements[] = {30'110 * m, 30'265 * m, 30'740 * m, 30'750 * m,
31'135 * m, 31'015 * m, 31'180 * m, 31'610 * m,
31'960 * m, 31'865 * m};
std::array gain = {0.2 * one, 0.1 * one};
print_header(initial);
example/kalman_filter/kalman_filter-example_3.cpp
+3 -2
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@@ -54,8 +54,9 @@ int main()
const auto interval = isq::duration(5 * s);
const state initial = {30 * km, 50 * (m / s)};
const quantity<isq::position_vector[m], int> measurements[] = {30'160 * m, 30'365 * m, 30'890 * m, 31'050 * m, 31'785 * m,
32'215 * m, 33'130 * m, 34'510 * m, 36'010 * m, 37'265 * m};
const quantity<isq::position_vector[m], int> measurements[] = {30'160 * m, 30'365 * m, 30'890 * m, 31'050 * m,
31'785 * m, 32'215 * m, 33'130 * m, 34'510 * m,
36'010 * m, 37'265 * m};
std::array gain = {0.2 * one, 0.1 * one};
print_header(initial);
example/kalman_filter/kalman_filter-example_4.cpp
+3 -2
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@@ -55,8 +55,9 @@ int main()
const auto interval = isq::duration(5. * s);
const state initial = {30 * km, 50 * (m / s), 0 * (m / s2)};
const quantity<isq::position_vector[m], int> measurements[] = {30'160 * m, 30'365 * m, 30'890 * m, 31'050 * m, 31'785 * m,
32'215 * m, 33'130 * m, 34'510 * m, 36'010 * m, 37'265 * m};
const quantity<isq::position_vector[m], int> measurements[] = {30'160 * m, 30'365 * m, 30'890 * m, 31'050 * m,
31'785 * m, 32'215 * m, 33'130 * m, 34'510 * m,
36'010 * m, 37'265 * m};
std::array gain = {0.5 * one, 0.4 * one, 0.1 * one};
print_header(initial);
example/si_constants.cpp
+10 -8
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@@ -36,19 +36,21 @@ int main()
std::cout << "The seven defining constants of the SI and the seven corresponding units they define:\n";
std::cout << UNITS_STD_FMT::format("- hyperfine transition frequency of Cs: {} = {:%.0Q %q}\n",
1. * si2019::hyperfine_structure_transition_frequency_of_cs,
(1. * si2019::hyperfine_structure_transition_frequency_of_cs)[Hz]);
1. * si2019::hyperfine_structure_transition_frequency_of_cs,
(1. * si2019::hyperfine_structure_transition_frequency_of_cs)[Hz]);
std::cout << UNITS_STD_FMT::format("- speed of light in vacuum: {} = {:%.0Q %q}\n",
1. * si2019::speed_of_light_in_vacuum, (1. * si2019::speed_of_light_in_vacuum)[m / s]);
1. * si2019::speed_of_light_in_vacuum,
(1. * si2019::speed_of_light_in_vacuum)[m / s]);
std::cout << UNITS_STD_FMT::format("- Planck constant: {} = {:%.8eQ %q}\n",
1. * si2019::planck_constant, (1. * si2019::planck_constant)[J * s]);
1. * si2019::planck_constant, (1. * si2019::planck_constant)[J * s]);
std::cout << UNITS_STD_FMT::format("- elementary charge: {} = {:%.9eQ %q}\n",
1. * si2019::elementary_charge, (1. * si2019::elementary_charge)[C]);
1. * si2019::elementary_charge, (1. * si2019::elementary_charge)[C]);
std::cout << UNITS_STD_FMT::format("- Boltzmann constant: {} = {:%.6eQ %q}\n",
1. * si2019::boltzmann_constant, (1. * si2019::boltzmann_constant)[J / K]);
1. * si2019::boltzmann_constant, (1. * si2019::boltzmann_constant)[J / K]);
std::cout << UNITS_STD_FMT::format("- Avogadro constant: {} = {:%.8eQ %q}\n",
1. * si2019::avogadro_constant, (1. * si2019::avogadro_constant)[1 / mol]);
1. * si2019::avogadro_constant, (1. * si2019::avogadro_constant)[1 / mol]);
// TODO uncomment the below when ISQ is done
// std::cout << UNITS_STD_FMT::format("- luminous efficacy: {} = {}\n", si2019::luminous_efficacy(1.),
// std::cout << UNITS_STD_FMT::format("- luminous efficacy: {} = {}\n",
// si2019::luminous_efficacy(1.),
// si2019::luminous_efficacy(1.)[lm / W]);
}
example/storage_tank_example.cpp
+2 -2
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@@ -103,8 +103,8 @@ int main()
using namespace mp_units::si::unit_symbols;
const auto height = isq::height(200 * mm);
auto tank = RectangularStorageTank(isq::length(1000 * mm), isq::width(500 * mm), height);
tank.set_contents_density(1000 * isq::mass_density[kg / m3]);
auto tank = RectangularStorageTank(isq::length(1'000 * mm), isq::width(500 * mm), height);
tank.set_contents_density(1'000 * isq::mass_density[kg / m3]);
const auto fill_time = 200 * s; // time since starting fill
const auto measured_mass = 20. * kg; // measured mass at fill_time
example/unmanned_aerial_vehicle.cpp
+2 -2
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@@ -162,6 +162,6 @@ int main()
};
waypoint wpt = {"EPPR", {54.24772_N, 18.6745_E}, msl_altitude{16. * ft}};
std::cout << UNITS_STD_FMT::format("{}: {} {}, {:%.2Q %q}, {:%.2Q %q}\n", wpt.name, wpt.pos.lat, wpt.pos.lon, wpt.msl_alt,
to_hae<earth_gravity_model::egm2008_1>(wpt.msl_alt, wpt.pos));
std::cout << UNITS_STD_FMT::format("{}: {} {}, {:%.2Q %q}, {:%.2Q %q}\n", wpt.name, wpt.pos.lat, wpt.pos.lon,
wpt.msl_alt, to_hae<earth_gravity_model::egm2008_1>(wpt.msl_alt, wpt.pos));
}