시험 MC_01 - 수동 모드

Objective

To test that manual flight modes work as expected

Preflight

Ensure that the drone can go into Stabilized, Altitude, Position mode while still on the ground

Flight Tests

❏ 안정화 상태

    ❏ Pitch/Roll/Yaw response 1:1

    ❏ Throttle response 1:1

❏ 고도

    ❏ Vertical position should hold current value with stick centered

    ❏ Pitch/Roll/Yaw response 1:1

    ❏ Throttle response set to Climbs/Descend rate

❏ 위치

    ❏ 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

❏ Landing

    ❏ Land in Position mode with the throttle below 40%

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

예상 결과

• 추력을 올릴 때 서서히 이륙한다
• 위에 언급한 어떤 비행 모드에서도 떨림이 나타나서는 안됨
• 지면에 착륙시, 콥터가 지면에서 튀면 안됨