MAVLink GUIDED Code
MAVLink GUIDED 波浪高度飞行任务
在前进过程中用正弦函数生成目标高度,演示水平速度与垂直速度的组合控制。
这些脚本用于学习和验证 ArduPilot/PX4 平台上的 pymavlink GUIDED 控制。实机测试前,请先在 SITL 或空旷安全环境验证,确认螺旋桨、GPS、EKF、遥控器接管、降落模式和急停流程都可用。
任务目标
起飞到 5 米高度,向前低速飞行,同时让高度在 4 到 6 米之间按正弦曲线变化,最后降落。
连接方式: 默认使用
udp:127.0.0.1:14550,适合 SITL 或本机 MAVLink 转发。实机使用时需要按自己的飞控串口或网络端口修改连接地址。学习重点
- 使用 math.sin 生成目标高度
- NED 坐标中 vz 为负表示上升、为正表示下降
- 适合测试高度控制、缓慢轨迹和传感器稳定性
脚本结构
| 函数 | 作用 |
|---|---|
connect() | 脚本流程中的控制步骤 |
set_mode() | 脚本流程中的控制步骤 |
wait_for_gps() | 脚本流程中的控制步骤 |
get_altitude() | 脚本流程中的控制步骤 |
wait_for_position_estimate() | 脚本流程中的控制步骤 |
arm() | 脚本流程中的控制步骤 |
takeoff() | 脚本流程中的控制步骤 |
send_velocity() | 脚本流程中的控制步骤 |
stop() | 脚本流程中的控制步骤 |
fly_wavy() | 脚本流程中的控制步骤 |
land() | 脚本流程中的控制步骤 |
main() | 核心任务函数 |
运行前检查
- 确认安装
pymavlink:pip install pymavlink - 确认飞控可以收到 GPS,并且 EKF 位置估计已经稳定。
- 确认遥控器可以随时切换模式或接管。
- 先拆桨做连接与解锁流程验证,再进入空旷环境低速测试。
完整代码:move_wavy.py
#!/usr/bin/env python3
import time
import math
from pymavlink import mavutil
def connect():
print(" Connecting...")
master = mavutil.mavlink_connection("udp:127.0.0.1:14550")
master.wait_heartbeat()
print(f" Connected: system={master.target_system}, component={master.target_component}")
return master
def set_mode(master, mode):
print(f" Setting mode: {mode}")
master.set_mode_apm(mode)
time.sleep(2)
def wait_for_gps(master):
print(" Waiting for GPS fix...")
while True:
msg = master.recv_match(type="GPS_RAW_INT", blocking=True, timeout=1)
if msg:
print(f"GPS fix_type={msg.fix_type}, satellites={msg.satellites_visible}")
if msg.fix_type >= 3 and msg.satellites_visible >= 8:
print(" GPS OK")
return
time.sleep(1)
def get_altitude(master):
msg = master.recv_match(type="GLOBAL_POSITION_INT", blocking=True, timeout=1)
if msg:
return msg.relative_alt / 1000.0
return None
def wait_for_position_estimate(master):
print(" Waiting for EKF position estimate / home...")
start = time.time()
while time.time() - start < 60:
msg = master.recv_match(
type=["EKF_STATUS_REPORT", "GLOBAL_POSITION_INT", "HOME_POSITION", "STATUSTEXT"],
blocking=True,
timeout=1
)
if not msg:
continue
if msg.get_type() == "GLOBAL_POSITION_INT":
alt = msg.relative_alt / 1000.0
print(f" Position estimate active, rel_alt={alt:.2f}m")
return
raise Exception(" No position estimate / home not ready")
def arm(master):
print(" Arming...")
while master.recv_match(blocking=False):
pass
master.mav.command_long_send(
master.target_system,
master.target_component,
mavutil.mavlink.MAV_CMD_COMPONENT_ARM_DISARM,
0,
1, 0, 0, 0, 0, 0, 0
)
start = time.time()
while time.time() - start < 15:
msg = master.recv_match(type=["HEARTBEAT"], blocking=True, timeout=1)
if msg and (msg.base_mode & mavutil.mavlink.MAV_MODE_FLAG_SAFETY_ARMED):
print(" Armed")
return
raise Exception(" Failed to arm automatically")
def takeoff(master, target_alt=5.0):
print(f" Taking off to {target_alt}m")
master.mav.command_long_send(
master.target_system,
master.target_component,
mavutil.mavlink.MAV_CMD_NAV_TAKEOFF,
0,
0, 0, 0, 0, 0, 0,
target_alt
)
while True:
alt = get_altitude(master)
if alt is not None and alt >= target_alt * 0.95:
print(" Target altitude reached")
break
time.sleep(0.2)
def send_velocity(master, vx=0, vy=0, vz=0):
master.mav.set_position_target_local_ned_send(
0,
master.target_system,
master.target_component,
mavutil.mavlink.MAV_FRAME_BODY_NED,
0b0000111111000111,
0, 0, 0,
vx, vy, vz,
0, 0, 0,
0, 0
)
def stop(master):
print(" Stopping")
for _ in range(20):
send_velocity(master, 0, 0, 0)
time.sleep(0.1)
def fly_wavy(master, center_alt=5.0, amplitude=1.0, duration=50.0, forward_speed=0.2):
print(" Flying wavy altitude pattern")
print(f" center_alt={center_alt}m amplitude={amplitude}m")
print(f" altitude range={center_alt - amplitude}m to {center_alt + amplitude}m")
wave_period = 10.0
max_vz = 0.4
altitude_gain = 0.6
start = time.time()
while time.time() - start < duration:
elapsed = time.time() - start
desired_alt = center_alt + amplitude * math.sin(2.0 * math.pi * elapsed / wave_period)
current_alt = get_altitude(master)
if current_alt is None:
send_velocity(master, vx=forward_speed, vy=0, vz=0)
time.sleep(0.1)
continue
altitude_error = desired_alt - current_alt
# In NED frame: negative vz goes up, positive vz goes down.
vz = -altitude_gain * altitude_error
vz = max(min(vz, max_vz), -max_vz)
send_velocity(master, vx=forward_speed, vy=0, vz=vz)
print(f"alt={current_alt:.2f}m target={desired_alt:.2f}m vz={vz:.2f}")
time.sleep(0.1)
stop(master)
def land(master):
print(" Landing...")
master.set_mode_apm("LAND")
master.motors_disarmed_wait()
print(" Disarmed")
def main():
master = connect()
wait_for_gps(master)
time.sleep(5)
wait_for_position_estimate(master)
set_mode(master, "GUIDED")
time.sleep(2)
arm(master)
takeoff(master, target_alt=5.0)
time.sleep(2)
fly_wavy(
master,
center_alt=5.0,
amplitude=1.0,
duration=50.0,
forward_speed=0.2
)
time.sleep(1)
land(master)
print(" Done")
if __name__ == "__main__":
main()
下一步
先从 10 米直线脚本开始,确认连接、解锁、起飞、速度控制和降落都稳定后,再测试圆形、8 字和波浪高度任务。