| Individual cell voltage | Measures the voltage of each cell or cell group in the battery pack. | Identifies cells that are approaching overvoltage or undervoltage limits before imbalance affects the pack. |
| Overvoltage protection | Stops or limits charging if a cell exceeds its permitted upper-voltage limit. | Helps reduce the risk of cell damage and unsafe charging. The applicable limit depends on cell chemistry and manufacturer specifications. |
| Undervoltage protection | Warns the flight controller or disconnects the load when a cell falls below its permitted lower-voltage limit. | Helps prevent excessive discharge, which can permanently damage rechargeable lithium cells and cause unexpected power loss. |
| Pack current | Measures charge and discharge current, often using a shunt or Hall-effect sensor. | Supports overload protection, power monitoring, and estimation of energy use during flight. |
| Overcurrent and short-circuit protection | Detects current above configured limits and can disable the battery output through a switching device. | Can protect the battery, wiring, and connected electronics from excessive current, subject to the pack’s protection design. |
| Cell and pack temperature | Uses temperature sensors to track battery temperature during charging, discharge, or storage. | Helps prevent operation outside the cell maker’s temperature limits and can trigger a warning or protective response. |
| Cell balancing | Reduces differences in cell voltage, typically by dissipating energy from higher-voltage cells or using an active balancing method. | Helps cells in a series-connected pack reach a more consistent charge level, improving usable pack capacity and supporting safer charging. |
| State of charge (SoC) | Estimates the remaining charge using voltage, current integration, and, where available, cell models. | Provides the pilot or flight controller with a battery-fuel estimate; accuracy depends on calibration, temperature, battery age, and load. |
| State of health (SoH) | Estimates battery condition from factors such as capacity change, internal resistance, and usage history. | Helps identify aging packs whose available capacity or power delivery may no longer meet flight requirements. |
| Communication and alerts | Sends battery data and fault status to compatible onboard systems through the selected interface. | Enables low-battery warnings, flight decisions, and post-flight diagnostics without adding unnecessary display hardware to the aircraft. |
| Compact, lightweight integration | Combines sensing, protection, and communication electronics in a small, low-mass design. | Helps preserve payload capacity and flight endurance while keeping battery monitoring close to the cells. |