DeltaQuad Evo Tactical Operations Manual
  • DeltaQuad Evo Tactical Edition
  • Safety and Legal Notice
  • Abbreviations
  • Vehicle Specifications
  • Auterion Suite
    • Create an Auterion Suite Account
    • Activating Your Vehicle
    • Using the DeltaQuad Evo Simulator
  • Setup
    • DeltaQuad Evo Flight Case
    • Field Deployment Kits
    • Assembly
    • DeltaQuad Evo Battery
      • Battery Handling
      • Charging the Battery
      • Storing the Battery
      • Main Battery Placement
      • Auxiliary Battery Placement
      • Empty Payload Box
    • Powering the Vehicle
    • Ground Control Station (GCS)
      • DeltaQuad Toughbook
      • Silvus StreamCaster 4240-EP
        • Attaching the Battery
        • Attaching the Antennas
        • Charging the Silvus Battery
        • Connecting the Breakout Cable
        • Storing the Silvus StreamCaster
      • Connecting the GCS to the DeltaQuad Evo
      • Optional Tripod-Mounted Sector Antenna
      • Optional Automated Tracking Antenna
        • Hardware Setup
        • Antenna Tracker GUI
        • Multivehicle Functionality
        • GCS Screen Recording
      • Silvus StreamCaster GUI
        • Changing the Radio Encryption
      • ATAK-Setup
    • Safety Features
      • Return to Home Settings
      • Low Battery Failsafe Trigger
      • Data Link Loss Failsafe Trigger
      • RC Loss Failsafe Trigger (Advanced Mode)
      • High Wind Failsafe Trigger
      • Geofence Failsafe Trigger
      • Land Mode Settings (Advanced Mode)
    • Air Unit Radio Swap
    • Connecting a Second GCS
    • ADS-B Receiver
  • Flight
    • Auterion Mission Control (AMC) Overview
      • Normal and Advanced Mode
      • AMC Top Bar
      • AMC Menu
        • Fly View
        • Plan View
        • Vehicle Overview
        • Advanced
        • Controller
        • Photos
        • Analyze
        • User Account
        • Settings
    • Planning a Mission
      • Preparing a Mission Plan
      • Best Practices and Tips
      • Mission Start Action
      • Set Intermediate Waypoints
        • Survey Pattern
        • Corridor Scan
        • Stealth Switch
      • Mission End Action
      • Geofences
    • Quick Takeoff
      • Land Approach
      • VTOL Takeoff
      • Return
    • Pre-flight Checks
    • Radio Range and Line of Sight (LOS) Operation
    • Executing and Monitoring a Mission
      • Execute the Mission - Returning the Vehicle
      • Monitoring the Mission
      • Controlling the Vehicle
      • Manual Control
      • Emergency Procedures
        • During Takeoff
        • During Transition
        • During Fixed-Wing Flight
        • During the Landing Sequence
    • Advanced Flight
      • GPS-Denied Operations
      • Offshore Operations
    • Post-flight Checks
  • Maintenance
    • Preventative maintenance
    • DeltaQuad Evo Maintenance Kit
      • VTOL Arm Replacement
      • Pusher Motor Pod Replacement
      • Wingtip Replacement
    • Elevon Replacement
    • Landing Gear Replacement
      • Landing Gear Leg Feature
    • Propeller Replacement
    • Flight Logs
      • Sharing log files via Auterion Suite
      • Downloading log files via the GCS
      • Downloading log files via USB
    • Diagnostics report
    • Firmware update
    • Compass calibration
    • Pitot Tube
  • DeltaQuad Evo Payloads
    • NextVision ISR Payloads
      • Raptor 360
      • Nighthawk2-V/UZ
      • Controlling the Camera
      • Connecting a Second Screen
      • NextVision Video Player
    • Aerial Payload Deployment Systems
    • Custom Payload Kits
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  1. Flight
  2. Executing and Monitoring a Mission
  3. Emergency Procedures

During Transition

The following should be monitored when the vehicle transitions from vertical flight to horizontal flight.

After reaching transition altitude, the vehicle will commence the transition to fixed-wing flight. The pusher motor will engage 5 meters below the target altitude (switching from quadcopter to fixed-wing). It will transition in the direction planned for takeoff, but wind can affect the direction, especially if the vehicle is not positioned with its nose directly into the wind.

The vehicle will engage high thrust using its pusher motor until it reaches the target airspeed. After this period, it should navigate towards the hold pattern or first waypoint.

If any malfunction occurs with the airspeed sensor, the vehicle will abort the transition after a timeout of 25 seconds. During this period, the vehicle can cover a long distance at the transition altitude. LAND mode must be engaged before the vehicle is at risk of colliding with any obstacles.

No Forward Motion

Operator Action: LAND

If the vehicle is not moving forward or is drifting with the wind and does not seem to transition towards fixed-wing, there is likely a problem with the pusher motor or propeller. The operator should review the propeller configuration as described in the manual.

Flying Backward

Operator Action: LAND

If the vehicle starts flying backward with increasing speed, the pusher propeller is likely mounted in the wrong direction. The transition should be aborted, and the pusher motor should be inspected.

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Last updated 7 months ago