feat: 初始化提交

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2026-01-30 18:50:52 +08:00
commit e251d681ab
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自动着陆.py Normal file
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from enum import Enum
import time
import krpc
from pid import PID
conn = krpc.connect(name='SpaceX Landing')
if not conn.space_center:
print("No active vessel found.")
exit()
# control = vessel.control
vessel = conn.space_center.active_vessel
celestial = vessel.orbit.body # 当前天体
# 创建 PID 控制器
# 外环:高度 -> 目标垂直速度(允许负值)
altitude_pid = PID(kp=0.3, ki=0.03, kd=0.05, integral_limit=2.0, alpha=0.8, output_limit=(-10.0, 10.0))
# 内环:垂直速度 -> 节流阀0~1
speed_pid = PID(kp=0.06, ki=0.05, kd=0.05, integral_limit=10.0, alpha=0.5, output_limit=(0.0, 1.0))
target_altitude = 30 # 目标高度,单位 m
# 状态机定义:高于 100m 为滑翔GLIDE100m 及以下为减速着陆LAND
class STATE(str, Enum):
GLIDE = "GLIDE"
LAND = "LAND"
current_state = STATE.GLIDE
last_time = time.monotonic()
loop_dt = 0.1
# 进入减速着陆时使用的目标垂直速度(保持原有行为)
target_vertical_speed = -3
try:
while True:
now = time.monotonic()
dt = now - last_time
last_time = now
flight = vessel.flight(vessel.orbit.body.reference_frame)
current_altitude = flight.surface_altitude
current_vertical_speed = flight.vertical_speed
# 计算转换距离
available_thrust = vessel.available_thrust # 可用推力
gav = celestial.surface_gravity # 重力加速度
twr = available_thrust / (vessel.mass * gav) # 推重比
if twr > 1.0:
transition_distance = (current_vertical_speed**2) / (2 * gav * (twr - 1)) # 米
else:
transition_distance = float('inf') # 无法减速,设为无穷大
# 状态判断:大于 200m 为滑翔(无需控制,油门 0否则为减速着陆使用现有内环 PID
if current_state == STATE.GLIDE: # 禁止反向切换
new_state = STATE.GLIDE if current_altitude > transition_distance else STATE.LAND
if new_state != current_state and new_state is not None:
print(f"状态切换: {current_state} -> {new_state}")
current_state = new_state
# 在状态切换时重置 PID避免积分风up
try:
altitude_pid.reset()
except Exception:
pass
try:
speed_pid.reset()
except Exception:
pass
if current_state == STATE.GLIDE:
# 滑翔:不做具体控制,油门设为 0
vessel.control.throttle = 0.0
print(f"当前高度: {current_altitude:.2f} m, 预计点火距离: {transition_distance:.2f} m, 状态: GLIDE, 油门: 0.00"," "*10, end='\r')
else:
# 内环:垂直速度误差 -> 节流阀
speed_error = target_vertical_speed - current_vertical_speed
throttle = speed_pid.update(speed_error, dt)
vessel.control.throttle = throttle
print(f"当前高度: {current_altitude:.2f} m, 预计点火距离: {transition_distance:.2f} m, 目标速: {target_vertical_speed:.2f} m/s, 速: {current_vertical_speed:.2f} m/s, 节流阀: {throttle:.2f}"," "*10, end='\r')
# 保持大致的控制周期
sleep_time = loop_dt - (time.monotonic() - now)
if sleep_time > 0:
time.sleep(sleep_time)
except KeyboardInterrupt:
vessel.control.throttle = 0.0
print("已停止控制,节流设为 0。")