From 1d86109d644bab2caed762de75f5688038a57f6e Mon Sep 17 00:00:00 2001
From: Armor <2654988228@qq.com>
Date: Tue, 1 Jul 2025 15:50:40 +0800
Subject: [PATCH] update

---
 config/config.json                          |   0
 requirements.txt                            | Bin 882 -> 1046 bytes
 src/KSP_tools/calculator_dv.py              | 120 +++++++++++---------
 src/KSP_tools/vessel_simulation_advanced.py |  18 ++-
 src/config/__init__.py                      |   0
 src/config/load_config.py                   |  25 ++++
 src/tools/novel_real.py                     |  41 +++++++
 7 files changed, 144 insertions(+), 60 deletions(-)
 create mode 100644 config/config.json
 create mode 100644 src/config/__init__.py
 create mode 100644 src/config/load_config.py
 create mode 100644 src/tools/novel_real.py

diff --git a/config/config.json b/config/config.json
new file mode 100644
index 0000000..e69de29
diff --git a/requirements.txt b/requirements.txt
index 551d13d938055e0ae5ba4602b18778d6594b975c..6023cbf52e1081ecf1b4facfb65f4978cfdefe53 100644
GIT binary patch
delta 173
zcmeywHjQIL5pz8+0~bRMLn1>SLpnn;Lk5tQ31sUs<TDg7qykwWejS4?g8_pcgE0^r
zF_<%e^b{~uGNgd@l>k*FgVh)T<qd&Q52~hwp%ADh7c6H26g2~igH#~dsfuE0GSJ#0
LptZ;rf;0gDbMPE2

delta 7
OcmbQn@ri9i5i<Y`8Unlk

diff --git a/src/KSP_tools/calculator_dv.py b/src/KSP_tools/calculator_dv.py
index 6bf4349..1b03b33 100644
--- a/src/KSP_tools/calculator_dv.py
+++ b/src/KSP_tools/calculator_dv.py
@@ -100,66 +100,74 @@ def cal_dv_step_by_step_fusion(reactor_efficiency, engine_efficiency, thrust, dr
 
 
 if __name__ == '__main__':
-    merlin_fuel_burned = cal_fuel_burned(314.3, 931, 1)
-    merlin_kinetic_energy = cal_kinetic_energy(314.3, 931, 1, 1)
-    theoretical_kerosene_burn_heat = 0.27785743459149853 * merlin_fuel_burned * 43.11 * 1000000
+    print(0.000005 * HYDROGEN_FUSION_EFFICIENCY * Vc * Vc / 3600/500)
 
-    raptor_fuel_burned = cal_fuel_burned(355, 2450, 1)
-    raptor_kinetic_energy = cal_kinetic_energy(355, 2450, 1, 1)
-    theoretical_methane_burn_heat = 0.20836197008574792 * raptor_fuel_burned * 55 * 1000000
+    light_speed_engine_power_requirement = cal_kinetic_energy(3000000, 4800, 1, 1)
+    # arc_reactor_power_output = 0.5*0.01*Vc*Vc
+    new_element_arc_output = 1*10**9
+    ratio = 1072*new_element_arc_output / light_speed_engine_power_requirement
+    print('111')
 
-
-    # first_stage_fuel = cal_fuel_burned(328, 812.05*4, 148)
-    # x = cal_fuel_burned(333, 80, 610) + cal_fuel_burned(350, 823.2, 148)
-    # x = cal_dv(338.2, 55000, 70000)
-    # xx = cal_fuel_burned(21000, 400, 1)
-
-    # payload_mass = 30
-    # structural_mass = 8
-    # return_fuel_mass = 8
-    # outbound_fuel_mass = 47
-    # return_dv = cal_dv(475, structural_mass, return_fuel_mass)
-    # out_bound_dv = cal_dv(475, payload_mass+structural_mass+return_fuel_mass, outbound_fuel_mass)
-    # total_mass = payload_mass + structural_mass + return_fuel_mass + outbound_fuel_mass
-
-    payload_mass = 45
-    structural_mass = 10
-    return_fuel_mass = 10
-    outbound_fuel_mass = 65
-    return_dv = cal_dv(475, structural_mass, return_fuel_mass)
-    out_bound_dv = cal_dv(475, payload_mass + structural_mass + return_fuel_mass, outbound_fuel_mass)
-    total_mass = payload_mass + structural_mass + return_fuel_mass + outbound_fuel_mass
-
-    # payload_mass = 30
+    # merlin_fuel_burned = cal_fuel_burned(314.3, 931, 1)
+    # merlin_kinetic_energy = cal_kinetic_energy(314.3, 931, 1, 1)
+    # theoretical_kerosene_burn_heat = 0.27785743459149853 * merlin_fuel_burned * 43.11 * 1000000
+    #
+    # raptor_fuel_burned = cal_fuel_burned(355, 2450, 1)
+    # raptor_kinetic_energy = cal_kinetic_energy(355, 2450, 1, 1)
+    # theoretical_methane_burn_heat = 0.20836197008574792 * raptor_fuel_burned * 55 * 1000000
+    #
+    #
+    # # first_stage_fuel = cal_fuel_burned(328, 812.05*4, 148)
+    # # x = cal_fuel_burned(333, 80, 610) + cal_fuel_burned(350, 823.2, 148)
+    # # x = cal_dv(338.2, 55000, 70000)
+    # # xx = cal_fuel_burned(21000, 400, 1)
+    #
+    # # payload_mass = 30
+    # # structural_mass = 8
+    # # return_fuel_mass = 8
+    # # outbound_fuel_mass = 47
+    # # return_dv = cal_dv(475, structural_mass, return_fuel_mass)
+    # # out_bound_dv = cal_dv(475, payload_mass+structural_mass+return_fuel_mass, outbound_fuel_mass)
+    # # total_mass = payload_mass + structural_mass + return_fuel_mass + outbound_fuel_mass
+    #
+    # payload_mass = 45
     # structural_mass = 10
-    # return_fuel_mass = 14
-    # outbound_fuel_mass = 71
-    # return_dv = cal_dv(382, structural_mass, return_fuel_mass)
-    # out_bound_dv = cal_dv(382, payload_mass + structural_mass + return_fuel_mass, outbound_fuel_mass)
+    # return_fuel_mass = 10
+    # outbound_fuel_mass = 65
+    # return_dv = cal_dv(475, structural_mass, return_fuel_mass)
+    # out_bound_dv = cal_dv(475, payload_mass + structural_mass + return_fuel_mass, outbound_fuel_mass)
     # total_mass = payload_mass + structural_mass + return_fuel_mass + outbound_fuel_mass
-
-    tank_mass = 0.000001 * 179380.1868 + 0.00003 * 41395.42773
-
-    x = cal_kinetic_energy(350, 2450, 1, 1)
-    # x = cal_kinetic_energy(314.3, 931, 1, 1)
-    y = cal_kinetic_energy(21000, 800, 1, 1)
-    print(y / x)
-    y = cal_fusion_input_mass(HYDROGEN_FUSION_EFFICIENCY * 0.1, x)
-
-    test = cal_burn_time(310, 1.95, 3)
-    ship_dry_mass = 2000*1000   # 2000t
-    ship_fuel_mass = 500*1000   # 500t
-    main_engine_thrust = 10000  # 10000KN
-    ship_isp, flow_rate = cal_best_isp_relativity_speed(reactor_efficiency=0.45, engine_efficiency=0.8,
-                                                        thrust=main_engine_thrust)
-    exhaust_velocity = ship_isp * Ga / Vc
-    dv = cal_dv(ship_isp, ship_dry_mass + ship_fuel_mass / 2, ship_fuel_mass / 2)
-    dv2 = cal_dv_step_by_step_fusion(reactor_efficiency=0.45, engine_efficiency=0.8, thrust=main_engine_thrust,
-                                     dry_mass=ship_dry_mass, fuel_mass=ship_fuel_mass, interval=1)
-    burn_time = ship_fuel_mass / flow_rate / 86400
-    x = 27632994.05705879
-
-    xxx = cal_fuel_burned(335.1, 1339.48, 174)
+    #
+    # # payload_mass = 30
+    # # structural_mass = 10
+    # # return_fuel_mass = 14
+    # # outbound_fuel_mass = 71
+    # # return_dv = cal_dv(382, structural_mass, return_fuel_mass)
+    # # out_bound_dv = cal_dv(382, payload_mass + structural_mass + return_fuel_mass, outbound_fuel_mass)
+    # # total_mass = payload_mass + structural_mass + return_fuel_mass + outbound_fuel_mass
+    #
+    # tank_mass = 0.000001 * 179380.1868 + 0.00003 * 41395.42773
+    #
+    # x = cal_kinetic_energy(350, 2450, 1, 1)
+    # # x = cal_kinetic_energy(314.3, 931, 1, 1)
+    # y = cal_kinetic_energy(21000, 800, 1, 1)
+    # print(y / x)
+    # y = cal_fusion_input_mass(HYDROGEN_FUSION_EFFICIENCY * 0.1, x)
+    #
+    # test = cal_burn_time(310, 1.95, 3)
+    # ship_dry_mass = 2000*1000   # 2000t
+    # ship_fuel_mass = 500*1000   # 500t
+    # main_engine_thrust = 10000  # 10000KN
+    # ship_isp, flow_rate = cal_best_isp_relativity_speed(reactor_efficiency=0.45, engine_efficiency=0.8,
+    #                                                     thrust=main_engine_thrust)
+    # exhaust_velocity = ship_isp * Ga / Vc
+    # dv = cal_dv(ship_isp, ship_dry_mass + ship_fuel_mass / 2, ship_fuel_mass / 2)
+    # dv2 = cal_dv_step_by_step_fusion(reactor_efficiency=0.45, engine_efficiency=0.8, thrust=main_engine_thrust,
+    #                                  dry_mass=ship_dry_mass, fuel_mass=ship_fuel_mass, interval=1)
+    # burn_time = ship_fuel_mass / flow_rate / 86400
+    # x = 27632994.05705879
+    #
+    # xxx = cal_fuel_burned(335.1, 1339.48, 174)
     print('done')
 
 
diff --git a/src/KSP_tools/vessel_simulation_advanced.py b/src/KSP_tools/vessel_simulation_advanced.py
index a6a3636..74ae23d 100644
--- a/src/KSP_tools/vessel_simulation_advanced.py
+++ b/src/KSP_tools/vessel_simulation_advanced.py
@@ -6,6 +6,8 @@ import time
 from matplotlib import pyplot as plt
 from tqdm import tqdm
 
+from calculator_dv import cal_dv
+
 Vc = 299792458
 Ga = 9.80665
 
@@ -257,6 +259,7 @@ if __name__ == '__main__':
                      176: 0.9, 177: 1, 180: 1, 190: 1},
     }
 
+
     # # CBC: 173s     S1: 227s    S2: 212s    S3: 800s
     # cbc_fuel_mass = 510000
     # cbc_dry_mass = 50000
@@ -300,9 +303,16 @@ if __name__ == '__main__':
     # Lanyue = Vessel([[S1], [S2]], name='Lanyue', payload=200, duration=0.05)
     # Lanyue.run_sim_new()
 
-    booster = Stage(163560, 16000, 4740, 285, 'solid', 'SRB')
-    S1 = Stage(350000, 25000, 3500, 456.5, 'hydrolox', 'Hydrolox Core Stage')
-    S2 = Stage(54000, 5000, 392, 450, 'hydrolox', 'Upper Stage')
-    SMART_LV = Vessel([[booster, S1], [S2]], name='SMART_LV', payload=20000, duration=0.05)
+    # booster = Stage(163560, 16000, 4740, 285, 'solid', 'SRB')
+    # S1 = Stage(350000, 25000, 3500, 456.5, 'hydrolox', 'Hydrolox Core Stage')
+    # S2 = Stage(54000, 5000, 392, 450, 'hydrolox', 'Upper Stage')
+    # SMART_LV = Vessel([[booster, S1], [S2]], name='SMART_LV', payload=20000, duration=0.05)
+    # SMART_LV.run_sim_new()
+
+    S1 = Stage(1200000, 300000, 1860*12, 452, 'hydrolox', 'Hydrolox Core Stage')
+    # S2 = Stage(200000, 20000, 1307, 448, 'hydrolox', 'J-2X Upper Stage')
+    S2 = Stage(250000, 20000, 2093, 460, 'hydrolox', 'RS-25-150 Upper Stage')
+    SMART_LV = Vessel([[S1], [S2]], name='SMART_LV', payload=30000, duration=0.05)
     SMART_LV.run_sim_new()
+    print('Stage 0 return dv:', cal_dv(452, 100000, 200000))
     print('done')
diff --git a/src/config/__init__.py b/src/config/__init__.py
new file mode 100644
index 0000000..e69de29
diff --git a/src/config/load_config.py b/src/config/load_config.py
new file mode 100644
index 0000000..9eee28d
--- /dev/null
+++ b/src/config/load_config.py
@@ -0,0 +1,25 @@
+import json
+import os
+
+from pathlib import Path
+
+from langchain_openai import ChatOpenAI
+from pydantic import SecretStr
+
+
+PROJECT_PATH = Path(__file__).parent.parent.parent.absolute()
+
+if os.path.exists(os.path.join(PROJECT_PATH, "config", "config_local.json")):
+    CONFIG_PATH = os.path.join(PROJECT_PATH, "config", "config_local.json")
+elif os.path.exists(os.path.join(PROJECT_PATH, "config", "config.json")):
+    CONFIG_PATH = os.path.join(PROJECT_PATH, "config", "config.json")
+else:
+    raise FileNotFoundError('Unable to locate config file, check src/config/config.json')
+
+
+with open(CONFIG_PATH, 'r', encoding='utf-8') as config_file:
+    project_config = json.load(config_file)
+
+
+LLM = ChatOpenAI(model=project_config['llm_model_name'], api_key= SecretStr(project_config['llm_secret_key']),
+                 base_url=project_config['llm_base_url'], temperature=0.01)
diff --git a/src/tools/novel_real.py b/src/tools/novel_real.py
new file mode 100644
index 0000000..a5a1b2b
--- /dev/null
+++ b/src/tools/novel_real.py
@@ -0,0 +1,41 @@
+import os
+
+from pathlib import Path
+
+PROJECT_PATH = Path(__file__).resolve().parent.parent.parent.absolute()
+DATA_PATH = os.path.join(PROJECT_PATH, 'data')
+
+def split_string(text, max_length):
+    """Splits a string into chunks, each with a maximum length.
+
+    Args:
+        text (str): The string to split.
+        max_length (int): The maximum length of each chunk.
+
+    Returns:
+        list: A list of strings, each with a length no more than max_length.
+    """
+    result = []
+    start = 0
+    while start < len(text):
+        end = min(start + max_length, len(text))
+        result.append(text[start:end])
+        start = end
+    return result
+
+novel_path = os.path.join(DATA_PATH, '如果，宅.txt')
+
+with open(novel_path, 'r', encoding='ANSI') as f:
+    novel = f.readlines()
+
+new_novel = ''
+for novel_line in novel:
+    line_list = split_string(novel_line, 30)
+    new_novel += '\n'.join(line_list)
+    new_novel += '\n'
+
+with open(os.path.join(DATA_PATH, 'target.txt'), 'w', encoding='utf-8') as f:
+    f.write(new_novel)
+
+
+print('done')
\ No newline at end of file