This is a comprehensive list of hot programming trends, and those that are declining in their popularity.
Need to modify existing designs of drones and aircraft to incorporate new technology.
I want to setup an environment to test Thermal Soaring of Fixed Wing UAV through Hardware In The Loop (HITL) simulation, inorder to test the features like, When the UAV experience Thermal , it circles around it, etc .
We want end-to-end NPNT to be implemented for Ardupilot including server setup. Tasks: 1 - Integrate NPNT lib into Ardupilot Resources: 2 - Develop and setup Drone registratiion/authentication server This should work e2e, we should have a backend where we can authorize a drone and view the drone logs and details as specified in the digitalsky specs. The user should be able to register the drone using UIN and the NPNT workflow should work. Resources: Resources: 3 - Integrate NPNT provisional testing tool 4 - Modify qgroundcontrol to talk with the auth server and complete the NPNT flow to allow arming (Open to discussion) References: This has almost every detail: Experience in Ardupilot is a plus, C++, Java must-have. We can discuss the tim...
I need someone who has experienced in COLMAP. C++ knowledge is a plus point. If you have worked on COLMAP, it will be helpful for me to hire. I need to modify the code when generating output. Lets discuss more.
There are lot of drones in the market where their communication protocol between the Remote control and the Drone are in open source community. There are some open source codes for intercepting the communication between the Drone and the Remote control and interpreting the Model Name and Number of the Drone. The proposed work here is to find out the majority of the drone vendor communication protocols data and developing simple C codes by which they can use the IQ data and extract the communication protocol that the drone is using. Detailed scope of work will be discussed on case to case based upon the individual's capability and background knowledge.
I'm looking for a mechanical or aerospace/aeronautical engineer to design an internal structure of a theoretical aircraft/drone given an external structure. In the front rotors there will be a maximum force of 250kg on each rotor and in the rear rotor the maximum force applied would be double than each front rotor. The overall weight should be 40-50kgs and should be able to carry under the belly 250kgs and around 120 Kgs more distributed on the rest of the structure. The materials used should be carbon fiber tubes (32mm external diameter and the attached connectors(images attached)) and alluminium tubes or cnc alluminium parts (further eventual connectors). To be noted that the external structure should be connected too. Note that in the shared file there are missing 4 legs that shou...