Modular personal transportation system
A vertical landing of an aircraft is performed using the first battery where the aircraft is unoccupied when the vertical landing is performed, the unoccupied aircraft includes the first battery, and the unoccupied aircraft excludes a second, removable battery. In response to detecting that the second, removable battery is detachably coupled to the aircraft, a power source for the aircraft is switched from the first battery to the second, removable battery. After switching the switch power source, a vertical takeoff of the aircraft is performed using the second, removable battery, wherein the aircraft is occupied when the vertical takeoff is performed.
1. A system, comprising:
a first battery; and
a controller which is configured to:
perform a vertical landing of an aircraft using a second, removable battery, wherein:
the aircraft is occupied by a passenger when the vertical landing is performed; and
the second, removable battery is detachably coupled to the occupied aircraft;
detect the second, removable battery being decoupled from the aircraft;
in response to detecting the second, removable battery being decoupled from the aircraft, switch a power source for the aircraft from the second, removable battery to the first battery, wherein the first battery has a smaller capacity than the second, removable battery and corresponds to a smaller load than the occupied aircraft; and
after switching the power source, perform a vertical takeoff of the aircraft using the first battery, wherein:
the aircraft is unoccupied when the vertical takeoff is performed;
the unoccupied aircraft includes the first battery; and
the unoccupied aircraft excludes the second, removable battery.
2. The system recited in claim 1 , wherein the aircraft further includes one or more of the following: a seat, a compartment for an occupant to stand in, a cockpit, a bicycle-style seat, a backless seat, or a saddle.
3. The system recited in claim 1 , wherein the aircraft further includes a seat and the second, removable battery is detachably coupled to the aircraft beneath the seat.
4. The system recited in claim 1 , wherein the aircraft further includes a compartment for an occupant to stand in and the second, removable battery is detachably coupled to the aircraft above the compartment.
5. The system recited in claim 1 , wherein:
the aircraft performs the vertical landing onto a docking station that enforces a single proper landing position for the aircraft; and
the second, removable battery is detachably coupled to the aircraft using the docking station.
6. The system recited in claim 1 , wherein:
the aircraft performs the vertical landing onto a docking station that enforces a single proper landing position for the aircraft and has an inwardly sloping side; and
the second, removable battery is detachably coupled to the aircraft using the docking station.
7. The system recited in claim 1 , wherein the second, removable battery includes two shoulder straps.
8. The system recited in claim 1 , wherein the second, removable battery includes a telescoping handle and a plurality of wheels.
9. The system recited in claim 1 , wherein the second, removable battery includes a male electrical plug with a retractable cord which is covered by a cap.
10. A method, comprising:
performing a vertical landing of an aircraft, wherein:
the aircraft is occupied by a passenger when the vertical landing is performed; and
the occupied aircraft includes a first battery and a second, removable battery; and
detecting the second, removable battery being decoupled from the aircraft;
in response to detecting the second, removable battery being decoupled from the aircraft, switching a power source for the aircraft from the second, removable battery to the first battery, wherein the first battery has a smaller capacity than the second, removable battery and corresponds to a smaller load than the occupied aircraft; and
after switching the power source, performing a vertical takeoff of the aircraft using the first battery, wherein the aircraft is unoccupied by a passenger when the vertical takeoff is performed.
11. The method recited in claim 10 , wherein the aircraft further includes one or more of the following: a seat, a compartment for an occupant to stand in, a cockpit, a bicycle-style seat, a backless seat, or a saddle.
12. The method recited in claim 10 , wherein the aircraft further includes a seat and the second, removable battery is detachably coupled to the aircraft beneath the seat.
13. The method recited in claim 10 , wherein the aircraft further includes a compartment for an occupant to stand in and the second, removable battery is detachably coupled to the aircraft above the compartment.
14. The method recited in claim 10 , wherein:
performing the vertical landing includes landing onto a docking station that enforces a single proper landing position for the aircraft; and
the second, removable battery is detachably coupled to the aircraft using the docking station.
15. The method recited in claim 10 , wherein:
performing the vertical landing includes landing onto a docking station that enforces a single proper landing position for the aircraft and has an inwardly sloping side; and
the second, removable battery is detachably coupled to the aircraft using the docking station.
16. The method recited in claim 10 , wherein the second, removable battery includes two shoulder straps.
17. The method recited in claim 10 , wherein the second, removable battery includes a telescoping handle and a plurality of wheels.
18. The method recited in claim 10 , wherein the second, removable battery includes a male electrical plug with a retractable cord which is covered by a cap.
19. A computer program product embodied in a non-transitory computer readable storage medium and comprising computer instructions for:
performing a vertical landing of an aircraft, wherein:
the aircraft is occupied by a passenger when the vertical landing is performed; and
the occupied aircraft includes a first battery and a second, removable battery; and
detecting the second, removable battery being decoupled from the aircraft;
in response to detecting the second, removable battery being decoupled from the aircraft, switching a power source for the aircraft from the second, removable battery to the first battery, wherein the first battery has a smaller capacity than the second, removable battery and corresponds to a smaller load than the occupied aircraft; and
after switching the power source, performing a vertical takeoff of the aircraft using the first battery, wherein the aircraft is unoccupied by a passenger when the vertical takeoff is performed.
20. The computer program product recited in claim 19 , wherein:
performing the vertical landing includes landing onto a docking station that enforces a single proper landing position for the aircraft; and
the second, removable battery is detachably coupled to the aircraft using the docking station.