Scenario: An agricultural technology company needs to survey a 500-hectare farm for crop health analysis. They must choose between two UAV configurations and determine if a single flight can cover the entire farm.
Given: - UAV maximum takeoff weight (MTOW): 25 kg - Empty weight: 12 kg - Battery options: Standard (4 kg, 45 min flight) or Extended (6 kg, 70 min flight) - Sensor options: - Multispectral camera only: 1.5 kg (NDVI analysis) - Multispectral + thermal: 3.2 kg (NDVI + water stress) - Multispectral + thermal + LiDAR: 6.5 kg (full canopy analysis) - Survey speed: 8 m/s at 100 m altitude - Swath width: 120 m with 20% overlap = 96 m effective
Steps: 1. Calculate available payload capacity: - With standard battery: 25 - 12 - 4 = 9 kg available - With extended battery: 25 - 12 - 6 = 7 kg available 2. Evaluate payload combinations: - Config A: Extended battery + full sensor suite = 6 + 6.5 = 12.5 kg > 7 kg available. NOT FEASIBLE - Config B: Standard battery + full sensor suite = 4 + 6.5 = 10.5 kg > 9 kg. NOT FEASIBLE - Config C: Extended battery + multispectral + thermal = 6 + 3.2 = 9.2 kg > 7 kg. NOT FEASIBLE - Config D: Standard battery + multispectral + thermal = 4 + 3.2 = 7.2 kg < 9 kg. FEASIBLE - Config E: Extended battery + multispectral only = 6 + 1.5 = 7.5 kg > 7 kg. NOT FEASIBLE - Config F: Standard battery + multispectral only = 4 + 1.5 = 5.5 kg < 9 kg. FEASIBLE 3. Calculate coverage per flight: - Config D (standard battery, 45 min): Coverage = 8 m/s x 45 min x 60 x 96 m = 2,073,600 m squared = 207 hectares - Config F (standard battery, 45 min): Same coverage = 207 hectares 4. Calculate flights needed for 500 hectares: 500 / 207 = 2.4 flights, so 3 flights minimum
Result: The optimal configuration is Config D (standard battery + thermal imaging), requiring 3 flights to cover the 500-hectare farm. Full LiDAR analysis would require a larger UAV platform (MTOW > 30 kg).
Key Insight: Payload capacity is the critical constraint in agricultural UAV operations, not battery life. Upgrading to an extended battery often backfires because the heavier battery reduces payload capacity.