Submitted:
12 August 2024
Posted:
13 August 2024
You are already at the latest version
Abstract
Keywords:
1. Introduction
2. Materials and Methods
- Combustion Cars: Mercedes Vito (2020), Renault Kangoo (2022), Peugeot 2008 (2021), 208 (2020), 308 (2023), VW Polo (2019), Citroen C3 (2022), Skoda Fabia (2019).
- Electric Cars: Specific models include Tesla Model 3 (2021) and Nissan Leaf (2020).
- Drone: Hybrid drone from Jedsy.ch with glider technology for maximal efficiency, transitioning to a hover mode for landing. (Table 1)
| Aircraft type | Unmanned electric aircraft, capable of vertical takeoff and landing (eVTOL) and fixed-wing flight. x |
| Dimensions | 35 x 290 x 240 cm [H x W x L] |
| Weight | 18 Kg empty incl. batteries |
| 21 Kg max. gross take-off weight (MGTOW) | |
| Propulsion | Hovering motors: 8x 150Kv motors with 22inch propellers (IP 45 rating) |
| Cruising motors: 2x 360Kv motors with 12inch propellers | |
| Avionics | 1x 64 Bit ARM 6 Cores, 6 MB L2 + 4 MB L3, 8 GB RAM, 128-Bit-LPDDR4x 59,7 GB/s |
| 1x 32 Bit ARM, 480MHz, 2MB memory, 512KB RAM | |
| 1x 32 Bit ARM, 24MHz, 8KB SRAM (3x Accelerometers/Gyros, 2x Barometers, 2x airspeed sensors, 1x GPS Module) | |
| 1x 32 Bit ARM, 480MHz, 2MB memory, 512KB RAM | |
| 1x 32 Bit ARM, 72MHz, 64KB SRAM (2x Accelerometers/Gyros, 2x Barometers, 1x GPS Module) | |
| Awareness systems | 1x downward-facing awareness systems |
| 2x forward-facing awareness systems | |
| 1x LiDAR ground altimeter: downward facing for long range | |
| Awareness radios | 1x ADS-B In |
| 1x FLARM in and out | |
| 1x remote ID, compliant with FAR Part 89 | |
| Connectivity (CON2) | 3x LTE SIM cards slots for three different providers |
| Flight modes | Multicopter mode and Fixed wing mode |
| Cruise Speed | 59 KIAS (30m/s) |
| Stall Speed (MGTOW) in Fixed Wing mode | 33 KIAS (17m/s) |
| Max Density Altitude | 2438m |
| Max Endurance | 118 minutes |
| Max Wind | 29 KTS (15m/s) |
| Max Precipitation | Light to moderate |
| Operating time | DayNight (under dev) |
| Operating temperature | -20° to 50° C |
| Range | max 120km, 2min hovering, 3kg payload, 5m/s of head wind, ideal cruising speed, 200m AMSL, no altitude changes or curves, 10% reserve |
| Weather limitations | suitable for operation in coastal and offshore climate |
| no operation during heavy rain, icing conditions, hail, and thunderstorms | |
| Noise Emissions | While cruising at 60m above ground level: 58dB |
| Delivery methods | Mailbox docking on balcony or window (under development) |
| Ground landing | |
| Customer Privacy | The video transmitted to the pilot for landing is blurred at the source |
| The recorded flight data is deleted and overwritten after every flight |
| Name of Route | Start and Destination | Start and Destination (GPS) |
| Route 1 | Buchs SG – Vaduz | 47.166668, 9.466664 - 47.134787, 9.513150 |
| Route 2 | Zürich Tiefenbrunnen – Zürich Oerlikon | 47.351448, 8.559639 - 47.406385, 8.542571 |
| Route 3 | Meilen – Zürich | 47.272483, 8.652122 - 47.351448, 8.559639 |
| Route 4 | Meilen – Rapperswil | 47.272483, 8.652122 - 47.220530, 8.843807 |
| Route 5 | Chur – Grüsch | 46.856858, 9.517722 - 46.977926, 9.644353 |
| Route 6 | Buchs SG – Mels | 47.166668, 9.466664 - 47.036573, 9.436659 |
| Route 7 | Glarus – Walenstadt | 47.036125, 9.065019 - 47.118043, 9.310155 |
| Route 8 | Buchs SG – Chur | 47.166668, 9.466664 - 46.856858, 9.517722 |
| Route 9 | Buchs SG – Stephanshorn SG | 47.166668, 9.466664 - 47.446111, 9.410633 |
| Name of Route | Start and Destination | Start and Destination (GPS) |
| Route 1 | Buchs SG – Gaflei | 47.166668, 9.466664 - 47.142344, 9.544172 |
| Route 2 | Meilen – Oetwil am See | 47.272483, 8.652122 - 47.267415, 8.728000 |
| Route 3 | Lugano - Bidogno | 46.023625, 8.961412 - 46.081164, 8.999985 |
| Route 4 | Buchs SG - Wildhaus | 47.166668, 9.466664 - 47.202323, 9.349811 |
| Route 5 | Buchs SG - Malbun | 47.166668, 9.466664 - 47.103642, 9.607433 |
| Route 6 | Chur - Arosa | 46.856858, 9.517722 - 46.784364, 9.683340 |
| Route 7 | Saas-Fee - Visp | 46.110250, 7.931477 - 46.297230, 7.874027 |
| Route 8 | Albula - Bonaduz | 46.663515, 9.575630 - 46.808014, 9.403732 |
| Route 9 | Davos - Landquart | 46.797116, 9.825824 - 46.961172, 9.566139 |
| cruising | Horizontally | 35m on each side of the Flight Path. This accounts for inaccuracy of the navigation due to GPS imprecision or meteorological conditions and allows the aircraft to safely maneuver within the margins of error. |
| cruising | Vertically | 20m above the Flight Path -> 120m AGL |
| hovering | Horizontally | 10m on each side of the flight path. This accounts for the low speed of the aircraft. |
| hovering | Vertically | 10m above the Flight Path -> 40m AGL This accounts for the low speed of the aircraft. |
| cruising | Horizontally | 35m on each side of the Flight Geography. This conservatively allows the aircraft to automatically initiate the Flight Geography contingency procedure to stop and hover from a cruise speed of 30m/s (approx. 26m), considering a positioning inaccuracy of 4m and an extra margin of 5m. |
| cruising | Vertically | 20m above the Flight Geography -> 150m AGL assuming 1s of reaction time at 45 deg pitch up at 20m/s + 4m of GPS error |
| hovering | Horizontally | 10m on each side of the Flight Geography. This accounts for the low speed of the aircraft. |
| hovering | Vertically | 10m above the Flight Geography -> 50m AGL This accounts for the low speed of the aircraft and the flight mode. |
- The RPIC activates the FTS using a mobile phone app (segregated from the GCS).
- The app sends the activation command through the mobile network to the FTS comms module installed on the aircraft (segregated from the C2 link and using a different network provider).
- The FTS comms module activates the FTS device.
- 4.
- Stabilize and stop the aircraft in Hovering mode as quickly as possible (approx. 4G deceleration)
- 5.
- Navigate to the horizontal GPS location where the FTS was triggered in Hovering mode at slow speed (5m/s),
- 6.
- Turn into the wind using the weathervane function to let the Cruising motor help in countering the wind more efficiently,
- 7.
- Slowly descend at 3m/s or less until touchdown,
- 8.
- Disarm the aircraft.

3. Results

4. Discussion
5. Conclusions
Supplementary Materials
Author Contributions
Acknowledgments
Conflicts of Interest
References
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