Files
omath/source/projectile_prediction/proj_pred_engine_avx2.cpp
2026-03-17 20:31:46 +03:00

270 lines
13 KiB
C++

//
// Created by Vlad on 2/23/2025.
//
#include "omath/projectile_prediction/proj_pred_engine_avx2.hpp"
#include <source_location>
#include <stdexcept>
#if defined(OMATH_USE_AVX2) && defined(__i386__) && defined(__x86_64__)
#include <immintrin.h>
#else
#include <format>
#endif
namespace omath::projectile_prediction
{
std::optional<Vector3<float>>
ProjPredEngineAvx2::maybe_calculate_aim_point([[maybe_unused]] const Projectile& projectile,
[[maybe_unused]] const Target& target) const
{
#if defined(OMATH_USE_AVX2) && defined(__i386__) && defined(__x86_64__)
const float bullet_gravity = m_gravity_constant * projectile.m_gravity_scale;
const float v0 = projectile.m_launch_speed;
const float v0_sqr = v0 * v0;
const Vector3 proj_origin = projectile.m_origin + projectile.m_launch_offset;
constexpr int SIMD_FACTOR = 8;
float current_time = m_simulation_time_step;
for (; current_time <= m_maximum_simulation_time; current_time += m_simulation_time_step * SIMD_FACTOR)
{
const __m256 times
= _mm256_setr_ps(current_time, current_time + m_simulation_time_step,
current_time + m_simulation_time_step * 2, current_time + m_simulation_time_step * 3,
current_time + m_simulation_time_step * 4, current_time + m_simulation_time_step * 5,
current_time + m_simulation_time_step * 6, current_time + m_simulation_time_step * 7);
const __m256 target_x
= _mm256_fmadd_ps(_mm256_set1_ps(target.m_velocity.x), times, _mm256_set1_ps(target.m_origin.x));
const __m256 target_y
= _mm256_fmadd_ps(_mm256_set1_ps(target.m_velocity.y), times, _mm256_set1_ps(target.m_origin.y));
const __m256 times_sq = _mm256_mul_ps(times, times);
const __m256 target_z = _mm256_fmadd_ps(_mm256_set1_ps(target.m_velocity.z), times,
_mm256_fnmadd_ps(_mm256_set1_ps(0.5f * m_gravity_constant), times_sq,
_mm256_set1_ps(target.m_origin.z)));
const __m256 delta_x = _mm256_sub_ps(target_x, _mm256_set1_ps(proj_origin.x));
const __m256 delta_y = _mm256_sub_ps(target_y, _mm256_set1_ps(proj_origin.y));
const __m256 delta_z = _mm256_sub_ps(target_z, _mm256_set1_ps(proj_origin.z));
const __m256 d_sqr = _mm256_add_ps(_mm256_mul_ps(delta_x, delta_x), _mm256_mul_ps(delta_y, delta_y));
const __m256 bg_times_sq = _mm256_mul_ps(_mm256_set1_ps(bullet_gravity), times_sq);
const __m256 term = _mm256_add_ps(delta_z, _mm256_mul_ps(_mm256_set1_ps(0.5f), bg_times_sq));
const __m256 term_sq = _mm256_mul_ps(term, term);
const __m256 numerator = _mm256_add_ps(d_sqr, term_sq);
const __m256 denominator = _mm256_add_ps(times_sq, _mm256_set1_ps(1e-8f)); // Avoid division by zero
const __m256 required_v0_sqr = _mm256_div_ps(numerator, denominator);
const __m256 v0_sqr_vec = _mm256_set1_ps(v0_sqr + 1e-3f);
const __m256 mask = _mm256_cmp_ps(required_v0_sqr, v0_sqr_vec, _CMP_LE_OQ);
const unsigned valid_mask = _mm256_movemask_ps(mask);
if (!valid_mask)
continue;
alignas(32) float valid_times[SIMD_FACTOR];
_mm256_store_ps(valid_times, times);
for (int i = 0; i < SIMD_FACTOR; ++i)
{
if (!(valid_mask & (1 << i)))
continue;
const float candidate_time = valid_times[i];
if (candidate_time > m_maximum_simulation_time)
continue;
// Fine search around candidate time
for (float fine_time = candidate_time - m_simulation_time_step * 2;
fine_time <= candidate_time + m_simulation_time_step * 2; fine_time += m_simulation_time_step)
{
if (fine_time < 0)
continue;
// Manually compute predicted target position to avoid adding method to Target
Vector3 target_pos = target.m_origin + target.m_velocity * fine_time;
if (target.m_is_airborne)
target_pos.z -= 0.5f * m_gravity_constant * fine_time * fine_time;
const auto pitch = calculate_pitch(proj_origin, target_pos, bullet_gravity, v0, fine_time);
if (!pitch)
continue;
const Vector3 delta = target_pos - proj_origin;
const float d = std::sqrt(delta.x * delta.x + delta.y * delta.y);
const float height = d * std::tan(angles::degrees_to_radians(*pitch));
return Vector3(target_pos.x, target_pos.y, proj_origin.z + height);
}
}
}
// Fallback scalar processing for remaining times
for (; current_time <= m_maximum_simulation_time; current_time += m_simulation_time_step)
{
Vector3 target_pos = target.m_origin + target.m_velocity * current_time;
if (target.m_is_airborne)
target_pos.z -= 0.5f * m_gravity_constant * current_time * current_time;
const auto pitch = calculate_pitch(proj_origin, target_pos, bullet_gravity, v0, current_time);
if (!pitch)
continue;
const Vector3 delta = target_pos - proj_origin;
const float d = std::sqrt(delta.x * delta.x + delta.y * delta.y);
const float height = d * std::tan(angles::degrees_to_radians(*pitch));
return Vector3(target_pos.x, target_pos.y, proj_origin.z + height);
}
return std::nullopt;
#else
throw std::runtime_error(
std::format("{} AVX2 feature is not enabled!", std::source_location::current().function_name()));
#endif
}
std::optional<AimAngles>
ProjPredEngineAvx2::maybe_calculate_aim_angles([[maybe_unused]] const Projectile& projectile,
[[maybe_unused]] const Target& target) const
{
#if defined(OMATH_USE_AVX2) && defined(__i386__) && defined(__x86_64__)
const float bullet_gravity = m_gravity_constant * projectile.m_gravity_scale;
const float v0 = projectile.m_launch_speed;
const Vector3 proj_origin = projectile.m_origin + projectile.m_launch_offset;
constexpr int SIMD_FACTOR = 8;
float current_time = m_simulation_time_step;
for (; current_time <= m_maximum_simulation_time; current_time += m_simulation_time_step * SIMD_FACTOR)
{
const __m256 times
= _mm256_setr_ps(current_time, current_time + m_simulation_time_step,
current_time + m_simulation_time_step * 2, current_time + m_simulation_time_step * 3,
current_time + m_simulation_time_step * 4, current_time + m_simulation_time_step * 5,
current_time + m_simulation_time_step * 6, current_time + m_simulation_time_step * 7);
const __m256 target_x
= _mm256_fmadd_ps(_mm256_set1_ps(target.m_velocity.x), times, _mm256_set1_ps(target.m_origin.x));
const __m256 target_y
= _mm256_fmadd_ps(_mm256_set1_ps(target.m_velocity.y), times, _mm256_set1_ps(target.m_origin.y));
const __m256 times_sq = _mm256_mul_ps(times, times);
const __m256 target_z = _mm256_fmadd_ps(_mm256_set1_ps(target.m_velocity.z), times,
_mm256_fnmadd_ps(_mm256_set1_ps(0.5f * m_gravity_constant), times_sq,
_mm256_set1_ps(target.m_origin.z)));
const __m256 delta_x = _mm256_sub_ps(target_x, _mm256_set1_ps(proj_origin.x));
const __m256 delta_y = _mm256_sub_ps(target_y, _mm256_set1_ps(proj_origin.y));
const __m256 d_sqr = _mm256_add_ps(_mm256_mul_ps(delta_x, delta_x), _mm256_mul_ps(delta_y, delta_y));
const __m256 delta_z = _mm256_sub_ps(target_z, _mm256_set1_ps(proj_origin.z));
const __m256 bg_times_sq = _mm256_mul_ps(_mm256_set1_ps(bullet_gravity), times_sq);
const __m256 term = _mm256_add_ps(delta_z, _mm256_mul_ps(_mm256_set1_ps(0.5f), bg_times_sq));
const __m256 term_sq = _mm256_mul_ps(term, term);
const __m256 numerator = _mm256_add_ps(d_sqr, term_sq);
const __m256 denominator = _mm256_add_ps(times_sq, _mm256_set1_ps(1e-8f));
const __m256 required_v0_sqr = _mm256_div_ps(numerator, denominator);
const __m256 v0_sqr_vec = _mm256_set1_ps(v0 * v0 + 1e-3f);
const __m256 mask = _mm256_cmp_ps(required_v0_sqr, v0_sqr_vec, _CMP_LE_OQ);
const unsigned valid_mask = _mm256_movemask_ps(mask);
if (!valid_mask)
continue;
alignas(32) float valid_times[SIMD_FACTOR];
_mm256_store_ps(valid_times, times);
for (int i = 0; i < SIMD_FACTOR; ++i)
{
if (!(valid_mask & (1 << i)))
continue;
const float candidate_time = valid_times[i];
if (candidate_time > m_maximum_simulation_time)
continue;
for (float fine_time = candidate_time - m_simulation_time_step * 2;
fine_time <= candidate_time + m_simulation_time_step * 2; fine_time += m_simulation_time_step)
{
if (fine_time < 0)
continue;
Vector3 target_pos = target.m_origin + target.m_velocity * fine_time;
if (target.m_is_airborne)
target_pos.z -= 0.5f * m_gravity_constant * fine_time * fine_time;
const auto pitch = calculate_pitch(proj_origin, target_pos, bullet_gravity, v0, fine_time);
if (!pitch)
continue;
const Vector3 delta = target_pos - projectile.m_origin;
const float yaw = angles::radians_to_degrees(std::atan2(delta.y, delta.x));
return AimAngles{*pitch, yaw};
}
}
}
for (; current_time <= m_maximum_simulation_time; current_time += m_simulation_time_step)
{
Vector3 target_pos = target.m_origin + target.m_velocity * current_time;
if (target.m_is_airborne)
target_pos.z -= 0.5f * m_gravity_constant * current_time * current_time;
const auto pitch = calculate_pitch(proj_origin, target_pos, bullet_gravity, v0, current_time);
if (!pitch)
continue;
const Vector3 delta = target_pos - projectile.m_origin;
const float yaw = angles::radians_to_degrees(std::atan2(delta.y, delta.x));
return AimAngles{*pitch, yaw};
}
return std::nullopt;
#else
throw std::runtime_error(
std::format("{} AVX2 feature is not enabled!", std::source_location::current().function_name()));
#endif
}
ProjPredEngineAvx2::ProjPredEngineAvx2(const float gravity_constant, const float simulation_time_step,
const float maximum_simulation_time)
: m_gravity_constant(gravity_constant), m_simulation_time_step(simulation_time_step),
m_maximum_simulation_time(maximum_simulation_time)
{
}
std::optional<float> ProjPredEngineAvx2::calculate_pitch([[maybe_unused]] const Vector3<float>& proj_origin,
[[maybe_unused]] const Vector3<float>& target_pos,
[[maybe_unused]] const float bullet_gravity,
[[maybe_unused]] const float v0,
[[maybe_unused]] const float time)
{
#if defined(OMATH_USE_AVX2) && defined(__i386__) && defined(__x86_64__)
if (time <= 0.0f)
return std::nullopt;
const Vector3 delta = target_pos - proj_origin;
const float d_sqr = delta.x * delta.x + delta.y * delta.y;
const float h = delta.z;
const float term = h + 0.5f * bullet_gravity * time * time;
const float required_v0_sqr = (d_sqr + term * term) / (time * time);
const float v0_sqr = v0 * v0;
if (required_v0_sqr > v0_sqr + 1e-3f)
return std::nullopt;
if (d_sqr == 0.0f)
return term >= 0.0f ? 90.0f : -90.0f;
const float d = std::sqrt(d_sqr);
const float tan_theta = term / d;
return angles::radians_to_degrees(std::atan(tan_theta));
#else
throw std::runtime_error(
std::format("{} AVX2 feature is not enabled!", std::source_location::current().function_name()));
#endif
}
} // namespace omath::projectile_prediction