| Operating band | 2.4 GHz ISM band | Frequency: 2,400 MHz | — | Choose a blade antenna specified for the intended 2.4 GHz channel range. | Check local frequency, power, and antenna-gain regulations before flight testing. |
| Transmitter output | 20 dBm conducted power | 100 mW before antenna and feed losses | — | Confirm that the radio can deliver its rated power across the selected channels. | Actual permitted radiated power depends on local regulations and system configuration. |
| UAV blade antenna gain | 2 dBi nominal | Assumed equal to the ground antenna gain | — | A moderate-gain blade is a practical starting point when the UAV changes heading and pitch. | Gain alone does not describe coverage; review the antenna pattern and orientation sensitivity. |
| Ground antenna gain | 2 dBi nominal | 2 dBi | — | Use a compatible polarization and keep the ground antenna clear of nearby obstructions. | A directional ground antenna may extend range but requires suitable pointing and tracking. |
| Combined cable and installation losses | 2 dB total | Includes feed, connector, and installation losses | — | Mount the blade as specified and minimize unnecessary coaxial cable length. | Measure or obtain real feed-loss figures for the installed system. |
| Illustrative Link-Budget Results |
| Low-rate, extended-range target | 1 Mbps PHY rate | Receiver sensitivity: −100 dBm; required fade margin: 10 dB | Approximately 4.0 km | A 2 dBi blade may be suitable for this target if the airframe and antenna pattern preserve adequate coverage. | Lower data rates often allow operation at weaker received signal levels. |
| Long-range control and telemetry | 6 Mbps PHY rate | Receiver sensitivity: −94 dBm; required fade margin: 10 dB | Approximately 2.0 km | Prioritize consistent antenna orientation and minimize shadowing from the battery, payload, and structure. | Use a separate control-link design where the mission requires independent link availability. |
| Moderate-rate video or payload data | 12 Mbps PHY rate | Receiver sensitivity: −90 dBm; required fade margin: 10 dB | Approximately 1.3 km | Check the blade’s radiation pattern over expected UAV bank and yaw angles. | Higher data rates generally require a stronger received signal and reduce the available range. |
| Higher-rate payload link | 24 Mbps PHY rate | Receiver sensitivity: −86 dBm; required fade margin: 10 dB | Approximately 0.8 km | Consider a higher-gain blade only after checking its pattern and coverage in all required flight attitudes. | A narrower or less uniform pattern can create dead zones despite a higher peak-gain rating. |
| High-rate, short-range target | 54 Mbps PHY rate | Receiver sensitivity: −80 dBm; required fade margin: 10 dB | Approximately 0.4 km | Favor a well-positioned, correctly polarized antenna and verify performance with the complete airframe. | These are PHY rates, not guaranteed application throughput. |
| Calculation Basis and Selection Checks |
| Free-space path-loss model | 2.4 GHz line-of-sight planning estimate | FSPL (dB) = 100.05 + 20 log10(distance in km) | Based on a 10 dB fade margin | Use the model as an initial comparison, not as a substitute for flight testing. | The model does not account for terrain, airframe shadowing, interference, or multipath fading. |
| Range calculation | 20 dBm transmitter; 2 dBi antennas at both ends; 2 dB combined losses | Maximum allowable path loss = transmitter power + antenna gains − losses − receiver sensitivity − fade margin | Values are rounded estimates | Update the calculation with the selected radio’s measured sensitivity and installed antenna gains. | Receiver sensitivity varies by radio, modulation, channel width, and packet-error criteria. |
| Polarization and mounting | Match antenna polarization at both ends | Account for polarization mismatch and installation effects in the link budget | Can reduce usable range | Follow the antenna’s intended mounting orientation and keep it away from conductive parts where possible. | Test the complete UAV, since the airframe and payload can alter antenna performance. |
| Final validation | Test across planned flight attitudes and operating distances | Record received signal level, packet loss, and achieved application throughput | Use the weakest observed condition for planning | Select the antenna that meets coverage needs with adequate margin, not simply the highest stated gain. | All ranges above are illustrative free-space estimates based on the stated assumptions. |
| Planning note: Receiver sensitivities and ranges are representative engineering assumptions for comparison, not guaranteed product specifications. Real-world range can be substantially lower because of interference, obstructions, antenna installation, regulatory limits, and flight dynamics. |