测试 MC_01 - 手动模式

解锁并起飞

❏ 设置飞行模式以稳定和布防

❏ 升高油门起飞

飞行

❏ 自稳

    ❏ Pitch/Roll/Yaw response 1:1

    ❏ Throttle response 1:1

❏ 高度

    ❏ Vertical position should hold current value with stick centered

    ❏ Pitch/Roll/Yaw response 1:1

    ❏ Throttle response set to Climbs/Descend rate

❏ 定点

    ❏ Horizontal position should hold current value with stick centered

    ❏ Vertical position should hold current value with stick centered

    ❏ Throttle response set to Climbs/Descend rate

    ❏ Pitch/Roll/Yaw response set to Pitch/Roll/Yaw rates

降落

❏ 降落位置模式，油门低于 40％

❏ Upon touching ground, copter should disarm automatically within 2 seconds (disarm time set by parameter: COM_DISARM_LAND)

预期成果

• 当油门升高时，起飞应该是平稳的
• 在上述任何飞行模式中都不应出现振荡
• 着陆时，直升机不应在地面上反弹