TY - GEN
T1 - Design, Analysis and Development of a Flying Wing UAV for Aerial Seeding and 3D Mapping
AU - Sai, Movva Srilakshmi
AU - Kumar, Kamlesh
AU - Prakash, Bhanu
N1 - Funding Information:
The project was completed with the full support of ?Centre of Excellence in Avionics and Navigation? Manipal Academy of Higher Education (MAHE), Manipal.
Publisher Copyright:
© 2020, Springer Nature Singapore Pte Ltd.
PY - 2020
Y1 - 2020
N2 - Unmanned aerial vehicle (UAV) commercialization has increased the possibility of performing monitoring, data collection, survey mapping and aerial seeding in the modern world. The main components used in unmanned aircraft systems are ground control station (GCS) which includes mission planner software and two-way communication system (Telemetry) between the GCS and the UAV, transmitter, and receiver, autopilot on board, payload, remote video terminal, etc. This paper deals with the entire design of flying wing UAV taking into account wing and fuselage design and later implementing payload attachment for aerial seeding and mapping. Initially, UAV has been designed using dimensions and wing loading parameters calculated from basic aerodynamics. The complete UAV was designed in CATIA, and flow and structural analysis was performed in ANSYS. UAV was fabricated using balsa wood to test the prototype. Modified UAV design is further fabricated using composite for aerial seeding.
AB - Unmanned aerial vehicle (UAV) commercialization has increased the possibility of performing monitoring, data collection, survey mapping and aerial seeding in the modern world. The main components used in unmanned aircraft systems are ground control station (GCS) which includes mission planner software and two-way communication system (Telemetry) between the GCS and the UAV, transmitter, and receiver, autopilot on board, payload, remote video terminal, etc. This paper deals with the entire design of flying wing UAV taking into account wing and fuselage design and later implementing payload attachment for aerial seeding and mapping. Initially, UAV has been designed using dimensions and wing loading parameters calculated from basic aerodynamics. The complete UAV was designed in CATIA, and flow and structural analysis was performed in ANSYS. UAV was fabricated using balsa wood to test the prototype. Modified UAV design is further fabricated using composite for aerial seeding.
UR - https://www.scopus.com/pages/publications/85081923175
UR - https://www.scopus.com/pages/publications/85081923175#tab=citedBy
U2 - 10.1007/978-981-15-2696-1_99
DO - 10.1007/978-981-15-2696-1_99
M3 - Conference contribution
AN - SCOPUS:85081923175
SN - 9789811526954
T3 - Lecture Notes in Mechanical Engineering
SP - 1023
EP - 1033
BT - Innovative Product Design and Intelligent Manufacturing Systems - Select Proceedings of ICIPDIMS 2019
A2 - Deepak, BBVL.
A2 - Parhi, DRK.
A2 - Jena, Pankaj C.
PB - Springer Gabler
T2 - 1st International Conference on Innovative Product Design and Intelligent Manufacturing System, ICIPDIMS 2019
Y2 - 17 May 2019 through 18 May 2019
ER -