| 1 | Define the battery voltage | Common compact UAV battery systems use 3S to 6S lithium-ion or lithium-polymer packs, equivalent to approximately 11.1–22.2 V nominal. | Support the exact cell count and chemistry, with cell-level voltage measurement and balancing suitable for the selected pack. | Match the BMS overvoltage and undervoltage thresholds to the battery manufacturer’s specified limits. Do not select a BMS only by nominal voltage. |
| 2 | Calculate continuous and peak current | A small multirotor may draw 10–25 A continuously and 30–60 A during takeoff or rapid maneuvering, depending on motors, propellers, and payload. | Provide continuous and peak discharge ratings with short-circuit, overcurrent, and overtemperature protection. | Choose a continuous rating above the measured maximum by a practical safety margin, and verify that peak current duration is adequate for takeoff and acceleration. |
| 3 | Account for payload and mission power | Cameras, LiDAR units, communication equipment, and delivery mechanisms can add approximately 5–30 W or more to the aircraft’s electrical load. | Offer accurate current and energy monitoring, separate load output protection, and sufficient connector and conductor capacity. | Estimate total power as propulsion power plus avionics and payload power. Confirm that the BMS does not limit essential payload or flight-control loads. |
| 4 | Match capacity to required flight time | A compact UAV pack may range from 2 Ah to 10 Ah. Usable capacity is lower than rated capacity because a reserve is needed to protect the battery and allow a safe landing. | Track state of charge using coulomb counting, voltage, current, temperature, and battery history where available. | Use the estimate: flight time in hours ≈ usable battery capacity in ampere-hours ÷ average current. Include a reserve rather than planning to use 100% of rated capacity. |
| 5 | Check weight and physical integration | For compact aircraft, every additional 50–100 g can affect payload capacity, power consumption, and flight endurance. | Use a lightweight board with suitable dimensions, mounting holes, thermal paths, and low-resistance power connections. | Confirm BMS mass, enclosure size, connector orientation, cable length, and clearance from motors, propellers, and other heat sources. |
| 6 | Define operating and charging conditions | Outdoor UAVs can experience cold starts, direct sunlight, vibration, moisture, and rapid temperature changes. Lithium batteries generally require controlled charging above freezing conditions. | Include multiple temperature sensors, charge and discharge temperature limits, cell balancing, and protection against abnormal charging conditions. | Verify the BMS temperature range, sensor placement, vibration resistance, moisture protection, and compatibility with the intended charger. |
| 7 | Select telemetry and safety functions | Flight controllers benefit from battery voltage, current, state of charge, remaining capacity, temperature, cycle count, and fault information. | Provide a suitable digital communication interface, fault logging, balancing status, and configurable protection thresholds. | Confirm protocol compatibility, update and configuration access, fail-safe behavior, and the ability to trigger low-battery or emergency-landing alerts. |