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refactor(example): glide computer refactored for V2
This commit is contained in:
@@ -27,7 +27,7 @@
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namespace glide_computer {
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using namespace units::isq;
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using namespace units;
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task::legs task::make_legs(const waypoints& wpts)
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{
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@@ -52,7 +52,7 @@ altitude terrain_level_alt(const task& t, const flight_point& pos)
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{
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const task::leg& l = t.get_legs()[pos.leg_idx];
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const height alt_diff = l.end().alt - l.begin().alt;
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return l.begin().alt + alt_diff * ((pos.dist - t.get_leg_dist_offset(pos.leg_idx)) / l.get_length()).common();
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return l.begin().alt + alt_diff * ((pos.dist - t.get_leg_dist_offset(pos.leg_idx)) / l.get_length());
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}
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// Returns `x` of the intersection of a glide line and a terrain line.
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@@ -61,7 +61,7 @@ altitude terrain_level_alt(const task& t, const flight_point& pos)
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distance glide_distance(const flight_point& pos, const glider& g, const task& t, const safety& s, altitude ground_alt)
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{
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const auto dist_to_finish = t.get_length() - pos.dist;
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return distance((ground_alt + s.min_agl_height - pos.alt).common() /
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return distance((ground_alt + s.min_agl_height - pos.alt) /
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((ground_alt - t.get_finish().alt) / dist_to_finish - 1 / glide_ratio(g.polar[0])));
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}
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@@ -85,7 +85,7 @@ flight_point takeoff(timestamp start_ts, const task& t) { return {start_ts, t.ge
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flight_point tow(timestamp start_ts, const flight_point& pos, const aircraft_tow& at)
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{
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const duration d = (at.height_agl / at.performance).common();
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const duration d = (at.height_agl / at.performance);
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const flight_point new_pos{pos.ts + d, pos.alt + at.height_agl, pos.leg_idx, pos.dist};
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print("Tow", start_ts, pos, new_pos);
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@@ -98,7 +98,7 @@ flight_point circle(timestamp start_ts, const flight_point& pos, const glider& g
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const height h_agl = agl(pos.alt, terrain_level_alt(t, pos));
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const height circling_height = std::min(w.cloud_base - h_agl, height_to_gain);
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const rate_of_climb circling_rate = w.thermal_strength + g.polar[0].climb;
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const duration d = (circling_height / circling_rate).common();
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const duration d = (circling_height / circling_rate);
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const flight_point new_pos{pos.ts + d, pos.alt + circling_height, pos.leg_idx, pos.dist};
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height_to_gain -= circling_height;
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@@ -114,7 +114,7 @@ flight_point glide(timestamp start_ts, const flight_point& pos, const glider& g,
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const auto new_distance = pos.dist + dist;
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const auto alt = ground_alt + s.min_agl_height;
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const auto l3d = length_3d(dist, pos.alt - alt);
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const duration d = l3d / g.polar[0].v.common();
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const duration d = l3d / g.polar[0].v;
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const flight_point new_pos{pos.ts + d, terrain_level_alt(t, pos) + s.min_agl_height, t.get_leg_index(new_distance),
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new_distance};
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@@ -126,7 +126,7 @@ flight_point final_glide(timestamp start_ts, const flight_point& pos, const glid
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{
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const auto dist = t.get_length() - pos.dist;
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const auto l3d = length_3d(dist, pos.alt - t.get_finish().alt);
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const duration d = l3d / g.polar[0].v.common();
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const duration d = l3d / g.polar[0].v;
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const flight_point new_pos{pos.ts + d, t.get_finish().alt, t.get_legs().size() - 1, pos.dist + dist};
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print("Final Glide", start_ts, pos, new_pos);
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@@ -151,7 +151,7 @@ void estimate(timestamp start_ts, const glider& g, const weather& w, const task&
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pos = tow(start_ts, pos, at);
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// estimate the altitude needed to reach the finish line from this place
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const altitude final_glide_alt = t.get_finish().alt + height(t.get_length().common() / glide_ratio(g.polar[0]));
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const altitude final_glide_alt = t.get_finish().alt + height(t.get_length() / glide_ratio(g.polar[0]));
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// how much height we still need to gain in the thermalls to reach the destination?
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height height_to_gain = final_glide_alt - pos.alt;
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@@ -23,26 +23,22 @@
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#pragma once
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#include "ranged_representation.h"
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#include <units/bits/external/hacks.h>
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#include <units/bits/fmt_hacks.h>
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#include <units/generic/angle.h>
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#include <units/isq/si/length.h>
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#include <units/quantity_kind.h>
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#include <units/isq/space_and_time.h>
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#include <units/quantity.h>
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#include <units/si/units.h>
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#include <compare>
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#include <limits>
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#include <numbers>
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#include <ostream>
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// IWYU pragma: begin_exports
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#include <compare>
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// IWYU pragma: end_exports
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namespace geographic {
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template<typename T = double>
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using latitude = units::angle<units::degree, ranged_representation<T, -90, 90>>;
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using latitude = units::quantity<units::isq::angular_measure[units::si::degree], ranged_representation<T, -90, 90>>;
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template<typename T = double>
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using longitude = units::angle<units::degree, ranged_representation<T, -180, 180>>;
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using longitude = units::quantity<units::isq::angular_measure[units::si::degree], ranged_representation<T, -180, 180>>;
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template<class CharT, class Traits, typename T>
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std::basic_ostream<CharT, Traits>& operator<<(std::basic_ostream<CharT, Traits>& os, const latitude<T>& lat)
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@@ -129,8 +125,7 @@ struct STD_FMT::formatter<geographic::longitude<T>> : formatter<T> {
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namespace geographic {
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struct horizontal_kind : units::kind<horizontal_kind, units::isq::si::dim_length> {};
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using distance = units::quantity_kind<horizontal_kind, units::isq::si::kilometre>;
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using distance = units::quantity<units::isq::distance[units::si::kilo<units::si::metre>]>;
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template<typename T>
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struct position {
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@@ -141,8 +136,8 @@ struct position {
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template<typename T>
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distance spherical_distance(position<T> from, position<T> to)
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{
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using namespace units::isq::si;
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constexpr length<kilometre> earth_radius(6371);
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using namespace units;
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constexpr auto earth_radius = 6371 * isq::radius[si::kilo<si::metre>];
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constexpr auto p = std::numbers::pi_v<T> / 180;
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const auto lat1_rad = from.lat.number() * p;
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@@ -159,13 +154,19 @@ distance spherical_distance(position<T> from, position<T> to)
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acos(sin(lat1_rad) * sin(lat2_rad) + cos(lat1_rad) * cos(lat2_rad) * cos(lon2_rad - lon1_rad));
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// const auto central_angle = 2 * asin(sqrt(0.5 - cos(lat2_rad - lat1_rad) / 2 + cos(lat1_rad) * cos(lat2_rad) * (1
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// - cos(lon2_rad - lon1_rad)) / 2));
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return distance(earth_radius * central_angle);
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// TODO can we improve the below
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// return quantity_cast<isq::distance>(earth_radius * central_angle);
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return earth_radius.number() * central_angle * isq::distance[earth_radius.unit];
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} else {
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// the haversine formula
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const auto sin_lat = sin((lat2_rad - lat1_rad) / 2);
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const auto sin_lon = sin((lon2_rad - lon1_rad) / 2);
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const auto central_angle = 2 * asin(sqrt(sin_lat * sin_lat + cos(lat1_rad) * cos(lat2_rad) * sin_lon * sin_lon));
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return distance(earth_radius * central_angle);
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// TODO can we improve the below
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// return quantity_cast<isq::distance>(earth_radius * central_angle);
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return earth_radius.number() * central_angle * isq::distance[earth_radius.unit];
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}
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}
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@@ -22,17 +22,12 @@
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#pragma once
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// IWYU pragma: begin_exports
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#include "geographic.h"
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#include <units/isq/si/length.h>
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#include <units/isq/si/speed.h>
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#include <units/isq/si/time.h>
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#include <units/quantity_point_kind.h>
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// IWYU pragma: end_exports
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#include <units/chrono.h>
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#include <units/format.h>
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#include <units/isq/space_and_time.h>
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#include <units/math.h> // IWYU pragma: keep
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#include <units/quantity_point.h>
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#include <algorithm>
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#include <array>
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#include <initializer_list>
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@@ -56,60 +51,43 @@
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// - no ground obstacles (i.e. mountains) to pass
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// - flight path exactly on a shortest possible line to destination
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template<units::QuantityKind QK>
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struct STD_FMT::formatter<QK> : formatter<typename QK::quantity_type> {
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template<typename FormatContext>
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auto format(const QK& v, FormatContext& ctx)
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{
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return formatter<typename QK::quantity_type>::format(v.common(), ctx);
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}
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};
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namespace glide_computer {
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template<units::QuantityKind QK1, units::QuantityKind QK2>
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constexpr units::Dimensionless auto operator/(const QK1& lhs, const QK2& rhs)
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requires(!units::QuantityKindRelatedTo<QK1, QK2>) && requires { lhs.common() / rhs.common(); }
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{
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return lhs.common() / rhs.common();
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}
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// kinds
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using horizontal_kind = geographic::horizontal_kind;
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struct vertical_kind : units::kind<vertical_kind, units::isq::si::dim_length> {};
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struct vertical_point_kind : units::point_kind<vertical_point_kind, vertical_kind> {};
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struct velocity_kind : units::derived_kind<velocity_kind, units::isq::si::dim_speed, horizontal_kind> {};
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struct rate_of_climb_kind : units::derived_kind<rate_of_climb_kind, units::isq::si::dim_speed, vertical_kind> {};
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// https://en.wikipedia.org/wiki/Flight_planning#Units_of_measurement
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inline constexpr struct mean_sea_level : units::absolute_point_origin<units::isq::height> {
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} mean_sea_level;
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QUANTITY_SPEC(rate_of_climb_speed, units::isq::height / units::isq::time);
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// length
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using distance = units::quantity_kind<horizontal_kind, units::isq::si::kilometre>;
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using height = units::quantity_kind<vertical_kind, units::isq::si::metre>;
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using altitude = units::quantity_point_kind<vertical_point_kind, units::isq::si::metre>;
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using distance = units::quantity<units::isq::distance[units::si::kilo<units::si::metre>]>;
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using height = units::quantity<units::isq::height[units::si::metre]>;
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using altitude = units::quantity_point<units::isq::altitude[units::si::metre], mean_sea_level>;
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// time
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using duration = units::isq::si::time<units::isq::si::second>;
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using timestamp = units::quantity_point<units::clock_origin<std::chrono::system_clock>, units::isq::si::second>;
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using duration = units::quantity<units::isq::duration[units::si::second]>;
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using timestamp =
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units::quantity_point<units::isq::time[units::si::second], units::chrono_point_origin<std::chrono::system_clock>{}>;
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// speed
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using velocity = units::quantity_kind<velocity_kind, units::isq::si::kilometre_per_hour>;
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using rate_of_climb = units::quantity_kind<rate_of_climb_kind, units::isq::si::metre_per_second>;
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using velocity = units::quantity<units::isq::speed[units::si::kilo<units::si::metre> / units::si::hour]>;
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using rate_of_climb = units::quantity<rate_of_climb_speed[units::si::metre / units::si::second]>;
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// text output
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template<class CharT, class Traits>
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std::basic_ostream<CharT, Traits>& operator<<(std::basic_ostream<CharT, Traits>& os, const altitude& a)
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{
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return os << a.relative().common() << " AMSL";
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return os << a.absolute() << " AMSL";
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}
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} // namespace glide_computer
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template<>
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struct STD_FMT::formatter<glide_computer::altitude> : formatter<units::isq::si::length<units::isq::si::metre>> {
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struct STD_FMT::formatter<glide_computer::altitude> :
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formatter<units::quantity<units::isq::altitude[units::si::metre]>> {
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template<typename FormatContext>
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auto format(glide_computer::altitude a, FormatContext& ctx)
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auto format(const glide_computer::altitude& a, FormatContext& ctx)
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{
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formatter<units::isq::si::length<units::isq::si::metre>>::format(a.relative().common(), ctx);
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formatter<units::quantity<units::isq::altitude[units::si::metre]>>::format(a.absolute(), ctx);
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return STD_FMT::format_to(ctx.out(), " AMSL");
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}
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};
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@@ -127,7 +105,10 @@ struct glider {
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std::array<polar_point, 1> polar;
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};
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constexpr units::Dimensionless auto glide_ratio(const glider::polar_point& polar) { return polar.v / -polar.climb; }
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constexpr units::weak_quantity_of<units::dimensionless> auto glide_ratio(const glider::polar_point& polar)
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{
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return polar.v / -polar.climb;
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}
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struct weather {
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height cloud_base;
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@@ -212,9 +193,10 @@ altitude terrain_level_alt(const task& t, const flight_point& pos);
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constexpr height agl(altitude glider_alt, altitude terrain_level) { return glider_alt - terrain_level; }
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inline units::isq::si::length<units::isq::si::kilometre> length_3d(distance dist, height h)
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inline units::quantity<units::isq::length[units::si::kilo<units::si::metre>]> length_3d(distance dist, height h)
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{
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return hypot(dist.common(), h.common());
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// TODO Should we be able to calculate this on quantity of different kinds? What to return?
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return hypot(quantity_cast<units::isq::length>(dist), quantity_cast<units::isq::length>(h));
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}
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distance glide_distance(const flight_point& pos, const glider& g, const task& t, const safety& s, altitude ground_alt);
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203
example/glide_computer_example.cpp
Normal file
203
example/glide_computer_example.cpp
Normal file
@@ -0,0 +1,203 @@
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// The MIT License (MIT)
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//
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// Copyright (c) 2018 Mateusz Pusz
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//
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// Permission is hereby granted, free of charge, to any person obtaining a copy
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// of this software and associated documentation files (the "Software"), to deal
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// in the Software without restriction, including without limitation the rights
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// to use, copy, modify, merge, publish, distribute, sublicense, and/or sell
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// copies of the Software, and to permit persons to whom the Software is
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// furnished to do so, subject to the following conditions:
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//
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// The above copyright notice and this permission notice shall be included in all
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// copies or substantial portions of the Software.
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//
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// THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR
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// IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY,
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// FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE
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// AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER
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// LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM,
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// OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE
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// SOFTWARE.
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#include "glide_computer.h"
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#include <units/bits/fmt_hacks.h>
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#include <units/chrono.h>
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#include <units/math.h>
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#include <units/si/international/length.h>
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#include <units/si/unit_symbols.h>
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#include <array>
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#include <exception>
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#include <iostream>
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#include <iterator>
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#include <string>
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#include <utility>
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#include <vector>
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namespace {
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using namespace glide_computer;
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using namespace units;
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auto get_gliders()
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{
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using namespace units::si::unit_symbols;
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UNITS_DIAGNOSTIC_PUSH
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UNITS_DIAGNOSTIC_IGNORE_MISSING_BRACES
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static const std::array gliders = {
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glider{"SZD-30 Pirat", {83 * isq::speed[km / h], -0.7389 * rate_of_climb_speed[m / s]}},
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glider{"SZD-51 Junior", {80 * isq::speed[km / h], -0.6349 * rate_of_climb_speed[m / s]}},
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glider{"SZD-48 Jantar Std 3", {110 * isq::speed[km / h], -0.77355 * rate_of_climb_speed[m / s]}},
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glider{"SZD-56 Diana", {110 * isq::speed[km / h], -0.63657 * rate_of_climb_speed[m / s]}}};
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UNITS_DIAGNOSTIC_POP
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return gliders;
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}
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auto get_weather_conditions()
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{
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using namespace units::si::unit_symbols;
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static const std::array weather_conditions = {
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std::pair{"Good", weather{1900 * isq::height[m], 4.3 * rate_of_climb_speed[m / s]}},
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std::pair{"Medium", weather{1550 * isq::height[m], 2.8 * rate_of_climb_speed[m / s]}},
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std::pair{"Bad", weather{850 * isq::height[m], 1.8 * rate_of_climb_speed[m / s]}}};
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return weather_conditions;
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}
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auto get_waypoints()
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{
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using namespace geographic::literals;
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using namespace units::si::international::unit_symbols;
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static const std::array waypoints = {
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waypoint{"EPPR", {54.24772_N, 18.6745_E}, altitude{16. * isq::altitude[ft]}}, // N54°14'51.8" E18°40'28.2"
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waypoint{"EPGI", {53.52442_N, 18.84947_E}, altitude{115. * isq::altitude[ft]}} // N53°31'27.9" E18°50'58.1"
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};
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return waypoints;
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}
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template<std::ranges::input_range R>
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requires(std::same_as<std::ranges::range_value_t<R>, glider>)
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void print(const R& gliders)
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{
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std::cout << "Gliders:\n";
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std::cout << "========\n";
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for (const auto& g : gliders) {
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std::cout << "- Name: " << g.name << "\n";
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std::cout << "- Polar:\n";
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for (const auto& p : g.polar) {
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const auto ratio = quantity_cast<one>(glide_ratio(g.polar[0]));
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std::cout << 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)
|
||||
quantity_cast<si::degree>(isq::asin(1 / ratio)));
|
||||
}
|
||||
std::cout << "\n";
|
||||
}
|
||||
}
|
||||
|
||||
template<std::ranges::input_range R>
|
||||
requires(std::same_as<std::ranges::range_value_t<R>, std::pair<const char*, weather>>)
|
||||
void print(const R& conditions)
|
||||
{
|
||||
std::cout << "Weather:\n";
|
||||
std::cout << "========\n";
|
||||
for (const auto& c : conditions) {
|
||||
std::cout << "- " << c.first << "\n";
|
||||
const auto& w = c.second;
|
||||
std::cout << " * Cloud base: " << STD_FMT::format("{:%.0Q %q}", w.cloud_base) << " AGL\n";
|
||||
std::cout << " * Thermals strength: " << STD_FMT::format("{:%.1Q %q}", w.thermal_strength) << "\n";
|
||||
std::cout << "\n";
|
||||
}
|
||||
}
|
||||
|
||||
template<std::ranges::input_range R>
|
||||
requires(std::same_as<std::ranges::range_value_t<R>, waypoint>)
|
||||
void print(const R& waypoints)
|
||||
{
|
||||
std::cout << "Waypoints:\n";
|
||||
std::cout << "==========\n";
|
||||
for (const auto& w : waypoints)
|
||||
std::cout << STD_FMT::format("- {}: {} {}, {:%.1Q %q}\n", w.name, w.pos.lat, w.pos.lon, w.alt);
|
||||
std::cout << "\n";
|
||||
}
|
||||
|
||||
void print(const task& t)
|
||||
{
|
||||
std::cout << "Task:\n";
|
||||
std::cout << "=====\n";
|
||||
|
||||
std::cout << "- Start: " << t.get_start().name << "\n";
|
||||
std::cout << "- Finish: " << t.get_finish().name << "\n";
|
||||
std::cout << "- Length: " << STD_FMT::format("{:%.1Q %q}", t.get_length()) << "\n";
|
||||
|
||||
std::cout << "- Legs: "
|
||||
<< "\n";
|
||||
for (const auto& l : t.get_legs())
|
||||
std::cout << STD_FMT::format(" * {} -> {} ({:%.1Q %q})\n", l.begin().name, l.end().name, l.get_length());
|
||||
std::cout << "\n";
|
||||
}
|
||||
|
||||
void print(const safety& s)
|
||||
{
|
||||
std::cout << "Safety:\n";
|
||||
std::cout << "=======\n";
|
||||
std::cout << "- Min AGL separation: " << STD_FMT::format("{:%.0Q %q}", s.min_agl_height) << "\n";
|
||||
std::cout << "\n";
|
||||
}
|
||||
|
||||
void print(const aircraft_tow& tow)
|
||||
{
|
||||
std::cout << "Tow:\n";
|
||||
std::cout << "====\n";
|
||||
std::cout << "- Type: aircraft\n";
|
||||
std::cout << "- Height: " << STD_FMT::format("{:%.0Q %q}", tow.height_agl) << "\n";
|
||||
std::cout << "- Performance: " << STD_FMT::format("{:%.1Q %q}", tow.performance) << "\n";
|
||||
std::cout << "\n";
|
||||
}
|
||||
|
||||
void example()
|
||||
{
|
||||
using namespace units::si::unit_symbols;
|
||||
|
||||
const safety sfty = {300 * isq::height[m]};
|
||||
const auto gliders = get_gliders();
|
||||
const auto waypoints = get_waypoints();
|
||||
const auto weather_conditions = get_weather_conditions();
|
||||
const task t = {waypoints[0], waypoints[1], waypoints[0]};
|
||||
const aircraft_tow tow = {400 * isq::height[m], 1.6 * rate_of_climb_speed[m / s]};
|
||||
// TODO use C++20 date library when available
|
||||
// set `start_time` to 11:00 am today
|
||||
const timestamp start_time(std::chrono::system_clock::now());
|
||||
|
||||
print(sfty);
|
||||
print(gliders);
|
||||
print(waypoints);
|
||||
print(weather_conditions);
|
||||
print(t);
|
||||
print(tow);
|
||||
|
||||
for (const auto& g : gliders) {
|
||||
for (const auto& c : weather_conditions) {
|
||||
std::string txt = "Scenario: Glider = " + g.name + ", Weather = " + c.first;
|
||||
std::cout << txt << "\n";
|
||||
std::cout << STD_FMT::format("{0:=^{1}}\n\n", "", txt.size());
|
||||
|
||||
estimate(start_time, g, c.second, t, sfty, tow);
|
||||
|
||||
std::cout << "\n\n";
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
} // namespace
|
||||
|
||||
int main()
|
||||
{
|
||||
try {
|
||||
example();
|
||||
} catch (const std::exception& ex) {
|
||||
std::cerr << "Unhandled std exception caught: " << ex.what() << '\n';
|
||||
} catch (...) {
|
||||
std::cerr << "Unhandled unknown exception caught\n";
|
||||
}
|
||||
}
|
@@ -24,6 +24,7 @@
|
||||
|
||||
#include "validated_type.h"
|
||||
#include <units/bits/external/hacks.h>
|
||||
#include <units/customization_points.h>
|
||||
#include <algorithm>
|
||||
#include <type_traits>
|
||||
|
||||
@@ -42,6 +43,9 @@ public:
|
||||
[[nodiscard]] constexpr ranged_representation operator-() const { return ranged_representation(-this->value()); }
|
||||
};
|
||||
|
||||
template<typename T, auto Min, auto Max>
|
||||
inline constexpr bool units::is_scalar<ranged_representation<T, Min, Max>> = units::is_scalar<T>;
|
||||
|
||||
template<typename T, auto Min, auto Max>
|
||||
struct std::common_type<std::intmax_t, ranged_representation<T, Min, Max>> :
|
||||
std::type_identity<ranged_representation<std::common_type_t<std::intmax_t, T>, Min, Max>> {};
|
||||
|
Reference in New Issue
Block a user