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Huace | Huayao P316- Aerial Survey Unmanned Aerial Vehicle Surveying System Vertical Takeoff and Autonomous Flight
Introduction - The new industrial grade flight control and navigation system of Huace Huayao P316 drone aerial survey system can ensure the autonomous
Product details
Huayao P316 UAV Aerial Survey System
The Huayao P316 adopts a modular hybrid layout, which can be flexibly assembled according to the specific situation of the field environment. The manual throwing/catapult parachute mode greatly improves the efficiency of drone operations, and the VTOL mode can quickly adapt to various complex environments.
The new industrial grade flight control and navigation system developed for the P316 series can ensure autonomous flight of the drone throughout the entire process. The takeoff and landing modes can be switched according to the assembly method, and it can be manually thrown, ejected, or vertically taken off. It can also parachute and vertically take off and land. Ensure that it can operate smoothly in terrain or densely populated areas such as plains, water bodies, mountains, hills, and jungles, and ensure high efficiency in data collection, truly achieving tool level unmanned aerial vehicles. The Huayao P316 drone has a wide range of applications in aviation surveying, pipeline inspection, emergency response, surveillance, and other fields.
The new industrial grade flight control and navigation system developed for the P316 series can ensure autonomous flight of the drone throughout the entire process. The takeoff and landing modes can be switched according to the assembly method, and it can be manually thrown, ejected, or vertically taken off. It can also parachute and vertically take off and land. Ensure that it can operate smoothly in terrain or densely populated areas such as plains, water bodies, mountains, hills, and jungles, and ensure high efficiency in data collection, truly achieving tool level unmanned aerial vehicles. The Huayao P316 drone has a wide range of applications in aviation surveying, pipeline inspection, emergency response, surveillance, and other fields.
|
project |
parameter |
|---|---|
|
Body length |
1m |
|
wingspan |
1.6m (1.66m in vertical mode) |
|
Machine weight |
4.3KG (6.5KG in vertical mode) |
|
Ceiling height |
Altitude 5000m (replace high-altitude components) |
|
Cruise speed |
18m/s-22m/s |
|
Drive Type |
Dual motor drive |
|
Actual payload |
800g |
|
Greater wind resistance capability |
Level 6 |
|
control distance |
10-60km |
|
Cruise time |
80 minutes (55 minutes in vertical mode) |
|
Takeoff method |
Hand throw, catapult, vertical takeoff |
|
landing method |
Drop, parachute drop |
|
Stall speed |
10m/s |
|
Typical homework efficiency |
Single flight of 7 square kilometers |
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