Synthesis of programmatic landing control algorithms for small UAV

1. Algorithm to find the optimal trajectory to land the UAV has been synthesized;
2. The controller has been synthesized to track the landing trajectory for small UAV in windy conditions.
The survey results reflect the correctness of the algorithm and show that the theoretical studies in the thesis have high reliability. The test results by simulation for a specific class of UAV (UAV-70V) have shown the correctness of the research results and the ability to apply the research results of the thesis in practice. The research results have contributed to supplementing and developing theory, and can be applied in the process of researching and manufacturing UAV as well as UAV control devices in Vietnam.