Long term evolution (LTE) air to ground communication enhancements associated with uplink synchronization

• US 9,929,794 B2
• Filed: 10/15/2015
• Issued: 03/27/2018
• Est. Priority Date: 10/15/2015
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Rowland, Andy
• Primary Examiner(s): NGUYEN, STEVEN H D
• Application Number:
  US14/884,561
• Publication Number:
  US 20170111103A1
• Time in Patent Office: 894 Days
• Field of Search: None
• CPC Class Codes: G01S 11/06 using intensity measurements
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service
• CPC Class Codes: H04W 56/0005 synchronizing of arrival of multiple uplinks
• CPC Class Codes: H04W 56/001 Synchronization between nodes
• CPC Class Codes: H04W 56/0045 compensating for timing error by altering transmission time
• CPC Class Codes: H04W 74/08 Non-scheduled access, e.g. ALOHA hybrid access H04W74/02

Abstract

A method for air to ground uplink synchronization comprises initiating a downlink synchronization of user equipment onboard an aircraft with a ground base station; computing a range to the base station based on a downlink path loss; selecting an initial time advance (TA) value from a set of predetermined TA values based on the range; and sending a first random access channel (RACH) request with the initial TA value to the base station in a first attempt to synchronize an uplink signal and attach the user equipment to a network. If the user equipment fails to attach, a next RACH request is sent with a next TA value to the base station, in a next attempt to synchronize the uplink signal and attach the user equipment to the network. If the user equipment fails again to attach, the method is repeated until the user equipment is attached to the network.

Claims

1. A method for air to ground uplink synchronization, the method comprising:

(a) initiating a downlink synchronization of user equipment onboard an aircraft with a ground base station, wherein at least a first antenna and a second antenna are mounted on the aircraft;

(b) computing a range to the ground base station based on a downlink path loss, wherein the downlink path loss is calculated independently for each of the first and second antennas;

(c) selecting an initial time advance value from a set of predetermined time advance values based on the computed range, wherein the initial time advance value is estimated from the antenna having the lowest downlink path loss;

(d) sending a first random access channel (RACH) request with the initial time advance value to the ground base station in a first attempt to synchronize an uplink signal and attach the user equipment to a network;

(e) if the user equipment fails to attach to the network, sending a next RACH request with a next time advance value from the set of predetermined time advance values to the ground base station, in a next attempt to synchronize the uplink signal and attach the user equipment to the network; and

(f) if the user equipment fails again to attach to the network, repeating step (e) until the user equipment is attached to the network with a current time advance value.

2. The method of claim 1, wherein when the user equipment is attached to the network, the method further comprising:

updating the current time advance value using the equation;

N_TA,new=N_TA,old+(TA−

31)*16,

where TA is the time advance value, N_TA is an integer index value of the TA, an amount of time alignment is given by N_TA=TA*16, N_TA,old is a current N_TA value, and N_TA,new is an updated N_TA value.

3. The method of claim 1, wherein the user equipment is configured for long term evolution (LTE) communications.

4. The method of claim 3, wherein the user equipment is in operative communication with a WiFi system onboard the aircraft, and the WiFi system is operatively connected to an LTE access gateway onboard the aircraft.

5. The method of claim 1, wherein the first antenna is co-located with the second antenna at a low elevation angle on the aircraft.

6. The method of claim 5, wherein a current next time advance value used in a current RACH request is decreased from a previous next time advance value used in a previous RACH request.

7. The method of claim 1, wherein the first antenna is mounted at the front of the aircraft, and the second antenna is mounted at the rear of the aircraft.

8. A computer program product, comprising:

a non-transitory computer readable medium having instructions stored thereon executable by a processor to perform a method for air to ground uplink synchronization, the method comprising;

(a) initiating a downlink synchronization of user equipment onboard an aircraft with a ground base station, wherein at least a first antenna and a second antenna are mounted on the aircraft;

(b) computing a range to the ground base station based on a downlink path loss, wherein the downlink path loss is calculated independently for each of the first and second antennas;

(c) selecting an initial time advance value from a set of predetermined time advance values based on the computed range, wherein the initial time advance value is estimated from the antenna having the lowest downlink path loss;

(d) sending a first random access channel (RACH) request with the initial time advance value to the ground base station in a first attempt to synchronize an uplink signal and attach the user equipment to a network;

(e) if the user equipment fails to attach to the network, sending a next RACH request with a next time advance value from the set of predetermined time advance values to the ground base station, in a next attempt to synchronize the uplink signal and attach the user equipment to the network; and

(f) if the user equipment fails again to attach to the network, repeating step (e) until the user equipment is attached to the network with a current time advance value.

9. A system for air to ground uplink synchronization, the system comprising:

a processor onboard an aircraft; and

a non-transitory computer readable medium having instructions stored thereon executable by the processor to perform a method comprising;

(a) initiating a downlink synchronization of user equipment onboard the aircraft with a ground base station, wherein at least a first antenna and a second antenna are mounted on the aircraft;

(b) computing a range to the ground base station based on a downlink path loss, wherein the downlink path loss is calculated independently for each of the first and second antennas;

(c) selecting an initial time advance value from a set of predetermined time advance values based on the computed range, wherein the initial time advance value is estimated from the antenna having the lowest downlink path loss;

(d) sending a first random access channel (RACH) request with the initial time advance value to the ground base station in a first attempt to synchronize an uplink signal and attach the user equipment to a network;

(e) if the user equipment fails to attach to the network, sending a next RACH request with a next time advance value from the set of predetermined time advance values to the ground base station, in a next attempt to synchronize the uplink signal and attach the user equipment to the network; and

(f) if the user equipment fails again to attach to the network, repeating step (e) until the user equipment is attached to the network with a current time advance value.

10. The system of claim 9, wherein when the user equipment is attached to the network, the method further comprising:

updating the current time advance value using the equation;

N_TA,new=N_TA,old+(TA−

31)*16,

where TA is the time advance value, N_TA is an integer index value of the TA, an amount of time alignment is given by N_TA=TA*16, N_TA,old is a current N_TA value, and N_TA,new is an updated N_TA value.

11. The system of claim 9, wherein:

the user equipment is configured for long term evolution (LTE) communications;

the user equipment is in operative communication with a WiFi system onboard the aircraft; and

the WiFi system is operatively connected to an LTE access gateway onboard the aircraft.

12. The system of claim 9, wherein when the first antenna is co-located with the second antenna at a low elevation angle on the aircraft, a current next time advance value used in a current RACH request is decreased from a previous next time advance value used in a previous RACH request.

13. The system of claim 9, wherein the first antenna is mounted at the front of the aircraft, and the second antenna is mounted at the rear of the aircraft.