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UAVs, Drones, eVTOL & Low-Altitude Aviation

Test Solutions for the Low-Altitude Economy

Programmable AC and DC sources, electronic loads, bidirectional source/sink systems, battery simulators, and modular measurement and I/O technology for aircraft, charging infrastructure, propulsion systems, BMS, avionics, and interconnection testing.

up to 2,400 V High-voltage load testing for next-generation platforms
42 kW / 3U Bidirectional DC power with energy recovery
0,5 mV Precise cell-voltage simulation for BMS testing
up to 1,100 A Current-pulse and ageing tests on cables
Full-Scenario Testing

From charging to signal-level testing

System-ready
Energy Charging & OBC
Powertrain DC/DC & Motor
Battery Pack & BMS
Electronics Avionics & I/O
Comprehensive Testing Approach

Three levels for an end-to-end test solution

Low-altitude aircraft combine high-voltage power electronics, highly dynamic propulsion systems, precise battery systems, and complex control and communication signals. The test system must reproduce these levels reliably and support full automation.

Power Management

Precise simulation of cell voltages, total voltage, total current, temperature, insulation resistance, and I/O signals for battery, BMS, and controller validation.

Power Testing

Grid simulation, battery and load emulation, high-voltage loading, load transients, and bidirectional energy flow for charging, DC/DC, and propulsion systems.

Electronic Testing

Modular power, measurement, and signal simulation for flight control, avionics, sensors, relays, CAN communication, PWM, cables, and connectors.

Research & Development Flexible test profiles, fault scenarios, dynamic measurements, and open interfaces.
Validation Reproducible testing of protection functions, efficiency, safety, and reliability.
Production & EOL Automated workflows, multi-channel technology, data logging, and report export.
System Integration Test instruments, switching system, EPO, interlock, measurement technology, and software from a single solution.
Applications

Test technology across the complete electric aircraft

From external charging infrastructure and high-voltage distribution to propulsion, BMS, flight control, sensors, cables, and connectors, the key components of a UAV or eVTOL system can be reproduced using scalable instruments and modular platforms.

01

Charging Infrastructure & Chargers

Grid, input, output, efficiency, power-factor, protection, and short-circuit testing of charging infrastructure for large and small aircraft.

N75500N35500N69200
02

Onboard Charger (OBC)

Simulation of the AC supply and battery pack for inrush current, ripple, efficiency, power factor, load dump, and protection-function testing.

N75500N35500N35100
03

DC/DC Converter

HV and LV input simulation, output loading, static characteristics, quiescent current, overshoot, recovery time, and short-circuit protection.

N38300N36200N69200
04

PMU, PDU & BDU

Supply, distribution, and protection testing of low-voltage power-management systems, high-voltage distribution units, and battery disconnect units.

N35500N35100N69200
05

Aircraft Battery

Charge/discharge cycling, capacity, ageing, voltage, current, and temperature testing for individual cells, modules, and complete battery packs.

N35500N35100NXI DAQ
06

Motor Controller

Battery simulation, inrush, regenerative energy, reverse current, CV/CC priority, and dynamic DC-link supply for electric propulsion systems.

N35500N35100NS81000
07

Flight Control & Avionics

Power supply, digital and analog I/O, CAN, relays, sensor excitation, measurement, and ground-offset testing for FCU, ECU, DCU, and VCU.

N36200NXIN2600
08

Aircraft BMS

Cell-voltage, total-voltage, current, temperature, insulation, and fault simulation for protection functions, SOC, balancing, and communication.

N9000N83624NXI
09

Harness & Connector

Dielectric strength, momentary interruption, short circuit, current cycling, overload, ageing, and temperature-rise testing of cables and connectors.

N36200N8150ANXI-6501
Typical System Architectures

Intelligently combine source, DUT, load, and signals

AC Grid Grid simulation Voltage, frequency, grid faults, and energy recovery
DUT Charging / OBC Input, efficiency, protection, and dynamic testing
DC Side Battery or load Bidirectional simulation or electronic load
Charging, OBC & DC/DC

Realistic energy flows on the AC and DC sides

For chargers, onboard chargers, and DC/DC converters, defined grid conditions, battery characteristics, and load profiles are combined. This enables reproducible testing of efficiency, power factor, start-up behavior, short circuit, overvoltage/undervoltage, and bidirectional operating modes.

Four-quadrantSource and regenerative load in one system
High VoltageLoad testing for next-generation voltage classes
DynamicsLoad steps, transients, and freely configurable sequences
Battery & BMS

From pack-level power to individual cell voltage

Bidirectional DC systems handle charge/discharge cycling and battery-pack simulation. Multi-channel battery simulators and modular measurement platforms add cell voltages, temperature-resistance simulation, total voltage, current-sensor signals, insulation resistance, fault scenarios, relays, and CAN communication.

0,5 mVHigh accuracy for cell and BMS validation
up to 36 channelsModular cell and temperature simulation
Fault scenariosOpen wire, short circuit, reverse polarity, and insulation faults
Pack levelBidirectional source/sink for charging, discharging, and SOC profiles
Cell levelMulti-channel cell-voltage simulation with galvanic isolation
TemperatureProgrammable resistors for NTC and sensor simulation
Fault simulationOpen-wire, short-circuit, polarity, and supply faults
CommunicationCAN, digital I/O, relays, and analog sensor signals
Power supplyProgrammable DC source with low ripple and waveform function
MeasurementAcquire voltage, current, temperature, and fast analog signals
I/O & PWMSimulate digital states, frequency, pulse width, and switching signals
SensorsPrecise source-measure functions for low currents and sensor signals
HarnessMomentary interruption, current cycling, short circuit, and temperature rise
Avionics, Sensors & Harness

Modular signal and measurement technology for complex electronics

NXI modules combine DAQ, relays, digital I/O, PWM, CAN, programmable resistors, and compact power functions. This creates scalable test systems for FCU, ECU, DCU, VCU, sensors, cables, and connectors—from the laboratory to end-of-line testing.

ModularConfigure functions to match the DUT
SynchronizedMulti-channel measurement and signal output
Automation-readyStandardized interfaces for test software and ATE
Selection Guide

Which solution fits each test application?

The table provides initial guidance. The final configuration depends on voltage, current, power, power flow, dynamics, accuracy, interfaces, test standards, safety concept, and the required level of automation.

Test Application Recommended Solution Typical Benefits
Charging Infrastructure / Charger N75500 / N35500 / N69200 Grid simulation, battery or aircraft emulation, output characteristics, efficiency, power factor, short circuit, and protection functions.
OBC / BOBC N75500 / N35500 / N35100 / N69200 AC input conditions, DC output, ripple, inrush, efficiency, load dump, A2G, and regenerative operation.
DC/DC Converter N38300 / N36200 / N35100 / N69200 HV/LV input simulation, output loading, quiescent current, overshoot, recovery time, and OVP, UVP, and short-circuit testing.
PMU / PDU / BDU N35500 / N35100 / N69200 / NXI Supply and load simulation, current cycling, power-up sequences, overload, ageing, fault detection, and protection logic.
Aircraft Battery N35500 / N35100 / NXI DAQ / NP301 Charge/discharge cycling, capacity, ageing, current, voltage, and temperature acquisition, plus safe battery-pack testing.
Motor Controller N35500 / N35100 / NS81000 Battery models, SOC profiles, regenerative energy, reverse current, start-up current, and stable DC-link supply with CV/CC priority.
Flight Control / Avionics N36200 / N8361F / N2600 / NXI ECU/FCU power supply, ground offset, sensor testing, digital and analog I/O, PWM, relays, CAN, and data acquisition.
Aircraft BMS N9000 / N83624 / N36200 / NXI Cell-voltage, total-voltage, current, temperature, insulation, and fault simulation for SOC, balancing, protection, and communication.
Harness & Connector N36200 / N8150A / NXI-6100 / NXI-6501 Momentary interruption, transient short circuit, current cycling, overload, temperature rise, and automated report export.
End-of-Line & Automated Systems Customized Test Stand Combination of source, load, battery simulator, DAQ, relays, CAN, safety technology, and test software for reproducible production testing.
From DUT to Test Stand

A structured path to the right low-altitude test solution

1. DUT Define the charging system, OBC, DC/DC converter, PDU, battery, inverter, BMS, FCU, or harness.
2. Key Specifications Record voltage, current, power, power flow, dynamics, accuracy, and insulation requirements.
3. Test Scenarios Describe profiles, fault scenarios, standards testing, endurance runs, temperature, and communication sequences.
4. Integration Define interfaces, switching matrix, interlock, EPO, measurement, software, and automation.
5. Solution Configure instrument selection, rack layout, safety concept, and test software together.
Project Consultation

Send us your UAV, drone, or eVTOL test requirements

ET System supports you in selecting suitable AC/DC test equipment and designing complete test stands. For an initial system concept, we ideally need the key electrical specifications, power flow, required dynamics, interfaces, and test sequences.

AC and DC voltage range
Maximum current, continuous power, and pulse power
Source, sink, or bidirectional operation
Battery, grid, or load simulation
Dynamics, slew rate, and test profiles
I/O, CAN, LAN, RS232, RS485, and analog signals
Interlock, EPO, insulation monitoring, and touch protection