IP Library › Granted Patent US 11,265,792
Granted Patent B2
US 11,265,792 · App. 16/638,413 · Granted Mar 1, 2022

Aerial vehicle state transition

Inventors: Jing Han (Beijing, CN); Lianhai Wu (Beijing, CN); Haiming Wang (Beijing, CN)
Assignee: Lenovo (Beijing) Co. LTD
H04W36/32H04W36/14H04W36/30
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Quick Facts
Patent No.
US 11,265,792
App. No.
16/638,413
Granted
Mar 1, 2022
Kind
B2
Abstract

Apparatuses, methods, and systems are disclosed for aerial vehicle state transition configuration. One apparatus ( 200 ) includes a receiver ( 212 ) that receives ( 902 ) a state transition configuration corresponding to an aerial vehicle from a base unit. The apparatus ( 200 ) includes a transmitter ( 210 ) that transmits ( 904 ) a state transition report to the base unit based on the state transition configuration.

Claims (57)

1. A method comprising:

receiving, at an aerial vehicle, a state transition configuration corresponding to the aerial vehicle, wherein the state transition configuration comprises at least one state transition condition that triggers transition between a ground state and an airborne state, the ground state and the airborne state have different radio configurations corresponding to interface control, mobility aspect, or a combination thereof, the ground state configures the aerial vehicle with parameters corresponding to a non-aerial vehicle, and the airborne state configures the aerial vehicle with parameters to reduce interference resulting from being airborne;

detecting, at the aerial vehicle, the at least one state transition condition;

transitioning, at the aerial vehicle, between the ground state and the airborne state in response to detecting the at least one state transition condition; and

transmitting, from the aerial vehicle, a state transition report based on the state transition configuration in response to transitioning between the ground state and the airborne state.

2. The method of claim 1 , wherein the state transition configuration comprises at least one state transition condition, and the at least one state transition condition comprises a first trigger that initiates transition to the ground state and a second trigger that initiates transition to the airborne state.

3. The method of claim 2 , wherein the at least one state transition condition comprises an altitude of the aerial vehicle passing a threshold altitude, a serving cellular network reference signal received power passing a threshold serving cellular network reference signal received power, a neighboring cellular network reference signal received power passing a threshold neighboring cellular network reference signal received power, an average of neighboring cellular network reference signal received powers passing a threshold average reference signal received power, a number of neighboring cellular networks passing a threshold number of neighboring cellular networks, or some combination thereof.

4. The method of claim 2 , wherein the first trigger that initiates transition to the ground state is selected from the group comprising:

an altitude of the aerial vehicle being less than a threshold altitude and a horizontal velocity of the aerial vehicle being less than a threshold horizontal velocity;

a number of neighboring cellular networks having a reference signal received power greater than a threshold reference signal received power being less than a threshold number; and

the altitude of the aerial vehicle being less than the threshold altitude and the number of neighboring cellular networks having a reference signal received power greater than the threshold reference signal received power being less than the threshold number.

5. The method of claim 2 , wherein the second trigger that initiates transition to the airborne state is selected from the group comprising:

an altitude of the aerial vehicle being greater than a threshold altitude and a horizontal velocity of the aerial vehicle being greater than a threshold horizontal velocity;

a number of neighboring cellular networks having a reference signal received power greater than a threshold reference signal received power being greater than a threshold number; and

the altitude of the aerial vehicle being greater than the threshold altitude and the number of neighboring cellular networks having a reference signal received power greater than the threshold reference signal received power being greater than the threshold number.

6. The method of claim 1 , wherein the state transition configuration comprises at least one conditional handover parameter, and the at least one conditional handover parameter comprises a first set of parameters for the ground state and a second set of parameters for the airborne state.

7. The method of claim 6 , wherein the first set of parameters comprises a neighboring cellular network having a reference signal received power better than a serving cellular network by a first offset, the second set of parameters comprises the neighboring cellular network having a reference signal received power better than the serving cellular network by a second offset, or some combination thereof.

8. The method of claim 1 , further comprising transmitting a response indicating that the state transition configuration is accepted in response to receiving the state transition configuration.

9. The method of claim 1 , further comprising:

determining whether one or more state transition conditions of the state transition configuration occur; and

transmitting the state transmission report in response to the one or more state transition conditions occurring.

10. The method of claim 1 , wherein the state transmission report comprises a current state, a measured altitude, a reference signal received power of a serving cellular network, a reference signal received power of a strongest neighboring cellular network, an average reference signal received power of neighboring cellular networks, a measured number of neighboring cellular networks, a measured number of neighboring cellular networks having a reference signal received power greater than a threshold reference signal received power, or some combination thereof.

11. The method of claim 1 , further comprising:

receiving a state transition command based on the state transition report; and

transmitting a report indicating completion of the state transition command.

12. The method of claim 1 , further comprising receiving a radio resource control configuration based on the state transition report, wherein the radio resource control configuration comprises a first handover command for a normal handover, a second handover command for a conditional handover, or a combination thereof.

13. The method of claim 12 , further comprising:

receiving the first handover command based on a state of the aerial vehicle;

in response to receiving the first handover command, performing a handover procedure; and

accessing a target base unit.

14. The method of claim 12 , further comprising:

receiving the second handover command based on a state of the aerial vehicle, wherein the second handover command comprises a trigger condition;

in response to receiving the second handover command, determining whether the trigger condition is triggered based on the state of the aerial vehicle;

in response to the trigger condition being triggered, performing a handover procedure; and

accessing a target base unit.

15. The method of claim 1 , further comprising:

receiving a handover procedure in response to transmitting the state transition report;

in response to execution of the handover procedure failing, transmitting a radio link failure report comprising state information of the aerial vehicle;

receiving an indication indicating that a base unit received the radio link failure report; and

receiving a handover report from the base unit.

16. The method of claim 1 , further comprising transmitting a measurement report based on a measurement.

17. The method of claim 16 , further comprising performing the measurement using a measurement configuration, wherein the measurement configuration comprises:

prior to the expiration of a timer, completing the measurement upon detection of a cell meeting predetermined criteria; and

upon expiration of the timer, measuring all detected cells.

18. The method of claim 16 , further comprising performing the measurement using a measurement configuration, wherein the measurement configuration comprises a maximum number of cells for which measurements are reported in the measurement report.

19. An apparatus comprising an aerial vehicle, the apparatus further comprising:

a receiver that receives a state transition configuration corresponding to the aerial vehicle, wherein the state transition configuration comprises at least one state transition condition that triggers transition between a ground state and an airborne state, the ground state and the airborne state have different radio configurations corresponding to interface control, mobility aspect, or a combination thereof, the ground state configures the aerial vehicle with parameters corresponding to a non-aerial vehicle, and the airborne state configures the aerial vehicle with parameters to reduce interference resulting from being airborne;

a processor that:

detects the at least one state transition condition; and

transitions between the ground state and the airborne state in response to detecting the at least one state transition condition; and

a transmitter that transmits a state transition report based on the state transition configuration in response to transitioning between the ground state and the airborne state.

20. A method comprising:

transmitting a state transition configuration corresponding to an aerial vehicle, wherein the state transition configuration comprises at least one state transition condition that triggers transition between a ground state and an airborne state, the ground state and the airborne state have different radio configurations corresponding to interface control, mobility aspect, or a combination thereof, the ground state configures the aerial vehicle with parameters corresponding to a non-aerial vehicle, and the airborne state configures the aerial vehicle with parameters to reduce interference resulting from being airborne; and

receiving a state transition report based on the state transition configuration in response to the aerial vehicle transitioning between the ground state and the airborne state as a result of the aerial vehicle detecting the at least one state transition condition.

21. An apparatus comprising:

a transmitter that transmits a state transition configuration corresponding to an aerial vehicle, wherein the state transition configuration comprises at least one state transition condition that triggers transition between a ground state and an airborne state, the ground state and the airborne state have different radio configurations corresponding to interface control, mobility aspect, or a combination thereof, the ground state configures the aerial vehicle with parameters corresponding to a non-aerial vehicle, and the airborne state configures the aerial vehicle with parameters to reduce interference resulting from being airborne; and

a receiver that receives a state transition report based on the state transition configuration in response to the aerial vehicle transitioning between the ground state and the airborne state as a result of the aerial vehicle detecting the at least one state transition condition.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 21, 2020
From: HAN, JING; WU, LIANHAI; WANG, HAIMING
To: LENOVO (BEIJING) CO. LTD
Reel/Frame 051892/0992 →
Continuity (1)
Related Publication 20200245215A1 · Jul 30, 2020