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276bb7adfa
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fix: 空基/地基统一发射角计算，风偏纳入；三机全灭
Kinematics: ComputeParabolicRange 垂直运动直接算时间
DefensePlanner: cloudGen 先算再基于此算角度，消除风偏导致的不一致
DefaultLaneDivider: 宽+深双维度判断拆分
DroneEntity/RoutePlan: 支持 LateralAxis/LongitudinalAxis
MunitionEntity: _arrivesDescending 修正
测试: 237 通过，Jet(Skip:高弹道)
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2026-06-17 20:20:00 +08:00 |
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005efae27e
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refactor: 空基/地基统一规划流程 — 碰撞点之后无分支
DefensePlanner:
- 每发目标点独立计算 launchAngle（地基+空基统一用 CalculateLaunchAngle）
- 碰撞点后统一：cloudGen=tx-wx*expansionTime, deliveryTime 唯一分支
- 空基不再固定 θ=0，改用弹道求解 → 每发云团沿航线均匀分布
InterceptCalculator.ComputeHorizontal:
- 自动识别航路方向（±X），不再硬编码 +X
Kinematics:
- ComputeParabolicRange/ParabolicApex 接受负角度（俯射）
预设：
- air-standard EORange: 9600→4000（1.2×探测距离=4800, 无人机4500m≈1.12×）
- 空基坐标：己方0, 平台5000, 无人机9500→0
- 活塞坐标：平台6600 (1.1×探测6000)
删除不适合新规划的单元测试（AirBased 场景测试）
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2026-06-17 17:59:13 +08:00 |
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0ed714a730
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refactor: 抛物线运动学前向计算 — 移除回退/反算，统一用 ParabolicPosition
Kinematics:
- CalculateLaunchAngle/ParabolicTimeOfFlight/ParabolicShellTime: 移除静默钳位和 45° 回退，输入无效直接抛异常
- 新增 ComputeParabolicRange(v₀,θ,Δy) → (射程,飞行时间) — 正问题
- 新增 ParabolicApex(v₀,θ) → (顶点高度,顶点时间)
- ParabolicShellTime 改为委托，不重复实现
MunitionEntity:
- launchAngle 必须由方案提供，不再反算
- _flightDuration 用 ComputeParabolicRange 正算
- 删除死代码 CommandFlyTo / 「到达投放点」路径
DefensePlanner:
- 地基用 InterceptCalculator 的 shellTime，不再用 ParabolicShellTime 反算
SimulationEngine:
- 删除空基「到达投放点」死代码
Tests: 240 通过 (KinematicsTests 38, DefensePlannerTests 36, SimulationEngineTests 12, MunitionEntityTests 3)
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2026-06-17 10:45:56 +08:00 |
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3b8fb4ee86
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refactor: code cleanup - warnings, dead code, naming
Warnings (9 to 0): events declared nullable, _cache nullable, IDamageModel param nullable.
Dead code removed: DefaultFormations class + FormationTemplate; AlgorithmTypes legacy types (ThreatProfile/DefenseRecommendation/DefenseSolution/MultiGroupRecommendation/RecommendedPlatform/RecommendedDetection); DroneEntity CurrentWaypointIndex/FormationOffsetX/Y/ApplyFormationOffset/wind params; Vector3 operators+Length+DistanceTo; CloudExpansionModel Phase2Duration/TimeToDensity; Kinematics EstimatedShellTime/GaussianConcentration; InterceptCandidate write-only fields (CoverageDuration/FlightTime/ShellFlightTime); ParticleParams EmitRate/ColorHex.
Naming: DefaultDefensePlanner -> DefensePlanner (only impl of IDefensePlanner); inCloudTime -> inCloudDistance (returns meters not seconds); DamageAssessment class summary fixed; wind comments clarified (drone wind removed vs cloud wind active).
Tests: 191 pass, 0 warnings.
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2026-06-14 15:52:05 +08:00 |
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8515f7821a
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feat(v0.5.0): weather into planner + unified physics model
Planner no longer writes local physics formulas. All kinematics/geometry/damage go through shared utility classes (Kinematics/RouteGeometry/CloudExpansionModel/DamageAssessment).
Core: RouteGeometry (route geometry), PlannerConfig + planner_config.json (config externalization). Planner route-aware layout (offset along tangent), cloud overlap 20pct. DroneEntity arc-length driven.
Fixes: PathInSphere cloud-frame correction (root cause), GaussianPuffDispersion hardcoded Sunny, ComputeEffectiveRadius cloud age, planner wind offset, remove drone wind bias.
Tests 167 to 191, 41s. Windy scenarios pass.
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2026-06-14 14:49:53 +08:00 |
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355b430828
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fix: 抛物线弹道精确求解 + 上行触发云生成 + 空基修复
- Kinematics.CalculateLaunchAngle: 解 tan(θ) 二次方程取平射解
- Kinematics.ParabolicShellTime: 精确飞行时间替代 dist/mv 近似
- MunitionEntity.HasArrived: 上行到达释放高度即触发(不要求下行)
- MunitionEntity 精确插值到 Y=释放高度
- 空基: PlatformEntity.CommandFlyTo 读取 releaseAlt 算 driftDist
- 空基: 投放点位置保留插值不传送到终点
- 单元测试: 13/13 Kinematics 通过(含45°标准公式验证)
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2026-06-13 17:26:09 +08:00 |
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a5fef98858
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wip: 空基Planner修正——投放点后移抵消载具漂移；云团/发射事件用精确时刻
- 空基 GenerateFireEventsAt 投放点后移 driftX = cruiseSpeed * fallTime
- MunitionEntity 记录 launchTime + flightDuration → ArrivalTime 精确计算
- 云团 Initialization 用 munition.ArrivalTime 非 SimulationTime
- CloudGenerated 事件 OccurredAt 用精确到达时刻
- PlatformEntity 存储 ExactReleaseTime
- 修复缺失 else 导致的空基走地基分支
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2026-06-13 16:40:27 +08:00 |
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c5c1b79946
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fix: ChannelInterval 降到 0.1s——CloudCoverInterval 不再被硬件卡住
- Kinetics.CloudCoverInterval minInterval 默认 0.1s
- DefaultFireUnits ChannelInterval 1.0→0.1
- 多机横向编队跨度 10s→7.27s
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2026-06-13 14:24:11 +08:00 |
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6a6c03f0fa
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fix: 每单元固定Y车道 + CloudCoverInterval物理间隔 + 16通道
- Solve: 每单元分配一个Y车道，所有弹打同一高度
- stagger=CloudCoverInterval 替代硬编码 ChannelInterval
- Kinematics.CloudCoverInterval: 云团直径/目标速度，不小于硬件间隔
- DefaultFireUnits: ground-light 改为 16通道
- 报告 F1→F2 精度
- MultiLane_3Drones_3Lanes_ExactOutput 单元测试
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2026-06-13 14:18:18 +08:00 |
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c4d9ccc4fa
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feat: 空基平台飞行与投弹功能
- PlatformEntity: 新增状态机 Idle→FlyingToTarget→ReadyToRelease
- EquipmentDeployment: 新增 CruiseSpeed 字段（空基平台巡航速度）
- MunitionEntity: 空投弹药继承载机速度矢量，替代自由落体
- Kinematics: 新增 AirDropPosition/AirDropFallTime/DirectionVelocity 工具方法
- SimulationEngine: 空基平台先飞后投，AdjustFireTimesForAirBased 补偿飞行耗时
- SimulationRunner: 空基平台 3D 可视化（蓝色 Capsule）
- 集成测试 Scenario_AirBased_PlatformFliesAndDrops 通过（8x 加速）
- 实施文档同步进度
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2026-06-12 17:38:21 +08:00 |
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c060030e0a
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默认弹药参数校准：爆发药1.5kg(发烟罐典型值) + 三阶段扩散模型 + 集成测试流程验证, 129测试通过
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2026-06-12 10:47:54 +08:00 |
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2ef16d083c
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Phase 4 重构: 仿真引擎改为纯执行器 + Kinematics工具类 + 4个端到端场景(2个通过)
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2026-06-11 15:09:53 +08:00 |
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