Skip to content
New issue

Have a question about this project? Sign up for a free GitHub account to open an issue and contact its maintainers and the community.

By clicking “Sign up for GitHub”, you agree to our terms of service and privacy statement. We’ll occasionally send you account related emails.

Already on GitHub? Sign in to your account

Update Fixed Wing Landing.md #10311

Merged
merged 1 commit into from
Aug 20, 2024
Merged
Changes from all commits
Commits
File filter

Filter by extension

Filter by extension

Conversations
Failed to load comments.
Loading
Jump to
Jump to file
Failed to load files.
Loading
Diff view
Diff view
2 changes: 1 addition & 1 deletion docs/Fixed Wing Landing.md
Original file line number Diff line number Diff line change
Expand Up @@ -15,7 +15,7 @@ This enables up to 4 different approach directions, based on the landing site an
3. The landing direction and the approach waypoints are calculated on the basis of the measured wind parameters. If no headwind landing is possible or the wind strength is greater than "Max. tailwind" (see Global Parameters), return to point 2.
4. The landing is initiated. The aircraft flies the downwind course, "Approach Altitude" is held.
5. Base Leg: the altitude is reduced from 2/3 of "Approach Altitude".
6. Final Appraoch: The engine power is reduced using "Pitch2throttle modifier" to reduce speed and the altitude is reduced to "Land Altitude".
6. Final Appraoch: The engine power is reduced using "Pitch2throttle modifier" to reduce speed and the altitude is gradually reduced towards "Land Altitude" while approaching the Safe Home Coordinates.
7. Glide: When "Glide Altitude" is reached, the motor is switched off and the pitch angle of "Glide Pitch" is held.
7. Flare: Only if a LIDAR/Rangefinder sensor is present: the motor remains switched off and the pitch angle of "Flare Pitch" is held
8. Landing: As soon as INAV has detected the landing, it is automatically disarmed, see setting `nav_disarm_on_landing`.
Expand Down