控制部分重构

This commit is contained in:
2026-06-01 14:26:39 +08:00
parent 00f4b84b65
commit a68f579a93
3 changed files with 275 additions and 4 deletions
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import time
import math
import threading
from pymavlink import mavutil
class DroneController:
def __init__(self, connection_string='/dev/ttyUSB0', baud=115200):
self.connection_string = connection_string
self.baud = baud
self.master = None
self.is_connected = False
# 飞控实时状态变量(多线程共享)
self.current_mode = None
self.is_armed = False
self.local_x = 0.0
self.local_y = 0.0
self.local_z = 0.0
self.roll = 0.0
self.pitch = 0.0
self.yaw = 0.0
# 线程控制开关
self.running = False
self.telemetry_thread = None
def connect(self):
"""初始化 MAVLink 串口连接,并等待首个心跳包"""
try:
print(f"正在尝试连接飞控 ({self.connection_string})...")
self.master = mavutil.mavlink_connection(self.connection_string, baud=self.baud)
self.master.wait_heartbeat(timeout=5)
self.is_connected = True
print("飞控连接成功,已接收到首个心跳包!")
# 开启后台线程,负责高频监听状态
self.running = True
self.telemetry_thread = threading.Thread(target=self._telemetry_loop, daemon=True)
self.telemetry_thread.start()
return True
except Exception as e:
print(f"连接飞控失败: {e}")
self.is_connected = False
return False
def _telemetry_loop(self):
"""后台线程:高频高吞吐量接收飞控状态反馈,刷新状态变量"""
while self.running and self.is_connected:
try:
# 阻塞式接收,超时 0.1 秒
msg = self.master.recv_match(blocking=True, timeout=0.1)
if not msg:
continue
msg_type = msg.get_type()
# 1. 解析心跳包获取模式与解锁状态
if msg_type == 'HEARTBEAT':
mode_id = msg.custom_mode
self.is_armed = bool(msg.base_mode & mavutil.mavlink.MAV_MODE_FLAG_SAFETY_ARMED)
# 尝试反向查找模式名称
if self.master:
# 寻找数值对应的模式字符串
for name, num in self.master.mode_mapping().items():
if num == mode_id:
self.current_mode = name
break
# 2. 解析局部 NED 位置坐标
elif msg_type == 'LOCAL_POSITION_NED':
self.local_x = msg.x # 北 (North)
self.local_y = msg.y # 东 (East)
self.local_z = msg.z # 地 (Down)
# 3. 解析姿态角 (弧度转角度)
elif msg_type == 'ATTITUDE':
self.roll = math.degrees(msg.roll)
self.pitch = math.degrees(msg.pitch)
self.yaw = math.degrees(msg.yaw)
except Exception as e:
print(f"\n遥测线程捕获到异常: {e}")
time.sleep(0.1)
def set_mode(self, mode_name):
"""切换飞控模式 (例如 GUIDED 或 OFFBOARD)"""
if not self.is_connected: return False
print(f"正在尝试切换到模式: {mode_name}...")
# 将模式名称转换为飞控可识别的内部数值
if mode_name not in self.master.mode_mapping():
print(f"错误,飞控不支持{mode_name}模式")
return False
mode_id = self.master.mode_mapping()[mode_name]
self.master.set_mode(mode_id)
print(f"已发送模式切换指令 -> {mode_name}")
return True
def arm(self):
"""发送解锁指令"""
if not self.is_connected: return False
print("正在发送解锁指令...")
self.master.mav.command_long_send(
self.master.target_system,
self.master.target_component,
mavutil.mavlink.MAV_CMD_COMPONENT_ARM_DISARM,
0, 1, 0, 0, 0, 0, 0, 0
)
# 等待并捕获飞控的 ACK 响应,超时时间设为 3 秒
ack = self.master.recv_match(type='COMMAND_ACK', blocking=True, timeout=3.0)
if ack and ack.command == mavutil.mavlink.MAV_COMMAND_ACK:
if ack.result == 0:
print(" ✅ [飞控通信] 飞控解锁成功 (Armed Success)!")
else:
print(f" ❌ [飞控通信] 飞控拒绝了解锁请求,拒绝代码 (Result): {ack.result}")
else:
print(" ⚠️ [飞控通信] 飞控未响应解锁确认,请检查飞控状态或数传指示灯。")
return True
def disarm(self):
"""发送上锁指令"""
if not self.is_connected: return False
print("正在发送强制上锁指令...")
self.master.mav.command_long_send(
self.master.target_system,
self.master.target_component,
mavutil.mavlink.MAV_CMD_COMPONENT_ARM_DISARM,
0, 0, 0, 0, 0, 0, 0, 0
)
return True
def send_body_velocity(self, vx, vy, vz, yaw_rate=0.0):
"""
核心控制接口:发送机体坐标系(Body Frame)下的速度指令
注意:在下发控制前,如果安全员人为切出了自主模式,则该函数拒绝发送,确保人肉兜底。
yaw_rate:单位(弧度/秒,rad/s),后续使用得转换为角度
"""
if not self.is_connected: return
if self.current_mode not in ['GUIDED', 'OFFBOARD']:
return
# 坐标系掩码定义:使用机体坐标系 (MAV_FRAME_BODY_NED)
# 掩码屏蔽:只保留 vx, vy, vz 和偏航速率 yaw_rate
coordinate_frame = mavutil.mavlink.MAV_FRAME_BODY_NED
type_mask = 0b0000111111000111 # 仅开放速度和偏航率
self.master.mav.set_position_target_local_ned_send(
0, # 系统时间戳(可传0)
self.master.target_system,
self.master.target_component,
coordinate_frame,
type_mask,
0, 0, 0, # 位置 (屏蔽)
vx, vy, vz, # 速度 (机体前后、机体左右、机体上下)
0, 0, 0, # 加速度 (屏蔽)
0, yaw_rate # 偏航,偏航率
)
def print_status(self):
"""利用 \r 实现终端单行丝滑刷新,动态打印 PID 命令与真实状态对比"""
print(
f"\r[Status] Armed: {self.is_armed} | "
f"Pos(N,E,D): ({self.local_x:+.2f}, {self.local_y:+.2f}, {self.local_z:+.2f}) | "
f"Yaw: {self.yaw:+.1f}°\033[K",
end="", flush=True
)
def close(self):
"""释放线程,关闭串口连接"""
self.running = False
if self.telemetry_thread:
self.telemetry_thread.join(timeout=1)
print("\n底层控制接口已安全断开。")
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import time
class PID:
"""
通用 PID 控制器类
封装了比例、积分、微分计算以及输出限幅、抗积分饱和功能
"""
def __init__(self, kp, ki, kd, max_out, min_out):
self.kp = kp
self.ki = ki
self.kd = kd
self.max_out = max_out
self.min_out = min_out
self.last_err = 0.0
self.integral = 0.0
self.last_time = time.time()
def update(self, error):
"""
根据当前误差计算 PID 输出
"""
current_time = time.time()
dt = current_time - self.last_time
if dt <= 0:
dt = 0.033 # 默认 30Hz 的更新步长
# 1. 比例项
p_out = self.kp * error
# 2. 积分项(增加累加计算,并对积分做出局部限幅防止初段积分饱和)
self.integral += error * dt
i_out = self.ki * self.integral
# 将积分上限限制在总输出幅值的 20%
i_out = max(min(i_out, self.max_out * 0.2), self.min_out * 0.2)
# 3. 微分项
d_out = self.kd * (error - self.last_err) / dt
# 4. 总输出合成
output = p_out + i_out + d_out
# 5. 总输出限幅
output = max(min(output, self.max_out), self.min_out)
# 保存状态供下次使用
self.last_err = error
self.last_time = current_time
return output
def reset(self):
"""
清空历史误差和积分,防止无人机在丢失目标重获后发生指令暴冲
"""
self.last_err = 0.0
self.integral = 0.0
self.last_time = time.time()