Monitoring system for an aircraft
A monitoring system 300 for an aircraft 100 including a controller 301 to determine, based on one or more conditions, one or more expected operating characteristics of a steering system of the aircraft. The one or more conditions include one or more aircraft conditions indicative of an internal condition of the aircraft and/or one or more external conditions indicative of an external influence on the aircraft. The controller compares the one or more expected operating characteristics with the one or more actual operating characteristics. The controller is configured to determine, based on the compare, whether to issue a signal indicating a condition of the aircraft. An avionics system 3000 comprising the monitoring system, an aircraft comprising the monitoring system or the avionics system, and a method 600 of monitoring an aircraft.
1. A system for an aircraft comprising at least one controller configured to:
based on one or more conditions, determine one or more expected operating characteristics of a steering system of the aircraft, the one or more expected operating characteristics being expected operating characteristics for controlling the aircraft on a surface to maintain the aircraft on a desired path along the surface, the one or more conditions comprising one or more aircraft conditions indicative of an internal condition of the aircraft and/or one or more external conditions indicative of an external influence on the aircraft;
automatically steer the aircraft using a steering system of the aircraft on the desired path;
determine that the aircraft is on the desired path;
in response to determining that the aircraft is on the desired path and while the aircraft is on the desired path, determine one or more actual operating characteristics under which the steering system is being operated to control the steering of the aircraft on the desired path;
perform a comparison process to compare the one or more expected operating characteristics with the one or more actual operating characteristics while the aircraft is on the desired path, wherein the comparison process includes a determination of whether an allowable range or threshold corresponding to the one or more actual operating characteristics is exceeded; and
determine, based on the comparison process and the determination of whether the one or more actual operating characteristics exceed the allowable range or threshold, whether to issue a signal indicating a condition of the aircraft relevant to the steering of the aircraft.
2. The system according to claim 1 , wherein the condition of the aircraft is indicative of an abnormal state of the steering system.
3. The system according to claim 1 , wherein the allowable range is an allowable range in which a nose gear wheel may be turned.
4. The system according to claim 1 , wherein the threshold is an amount of rudder trim.
5. The system according to claim 1 , wherein the signal comprises an audio-visual output.
6. The system according to claim 1 , wherein the controller is configured to determine, based on the comparison process, whether to issue the signal indicating a condition of the aircraft and transmit information about the comparison process to a recorder.
7. The system according to claim 1 , wherein the signal comprises a command to adjust a control parameter of the aircraft.
8. The system according to claim 1 , wherein the one or more external conditions comprises an indication of a wind speed generated by a wind speed sensor and/or a wind direction generated by a wind direction sensor arranged to determine a wind direction with respect to a longitudinal axis of the aircraft.
9. The system according to claim 1 , wherein the one or more aircraft conditions comprises an indication of a weight and/or a center of gravity of the aircraft.
10. The system according to claim 1 , the one or more aircraft conditions comprises an indication of an amount of thrust from a starboard engine of the aircraft and an amount of thrust from a port engine of the aircraft.
11. The system according to claim 1 , wherein the one or more aircraft conditions comprises an indication of an amount of braking from a starboard brake of the aircraft and an amount of braking from a port brake of the aircraft.
12. An avionics system comprising the system according to claim 1 .
13. An aircraft comprising the system according to claim 1 .
14. A method comprising:
determining, based on one or more conditions, one or more expected operating characteristics of a steering system of the aircraft, the one or more expected operating characteristics being expected operating characteristics for controlling the aircraft on a surface to maintain the aircraft on a desired path along the surface, the one or more conditions comprising one or more aircraft conditions indicative of an internal condition of the aircraft and/or one or more external conditions indicative of an external influence on the aircraft;
automatically steer the aircraft using a steering system of the aircraft on the desired path;
determine that the aircraft is on the desired path;
in response to determining that the aircraft is on the desired path and while the aircraft is on the desired path, determine one or more actual operating characteristics under which the steering system is being operated to control the steering of the aircraft on the desired path;
comparing the one or more expected operating characteristics with the one or more actual operating characteristics while the aircraft on the desired path along the surface;
determining, based on the comparison, whether a range or threshold corresponding to the one or more actual operating characteristics is exceeded; and
determining, based on the determination of whether the range or the threshold is exceeded, whether to issue a signal indicating a condition of the aircraft relevant to the steering of the aircraft.
15. An aircraft assistance device for assisting operation of an aircraft, the aircraft assistance device comprising one or more processors configured to:
obtain at least one predicted steering command according to a detection of at least one aircraft operation parameter and/or at least one environmental parameter;
automatically steer the aircraft using a steering system of the aircraft on a desired path along a surface;
determine that the aircraft is on the desired path; and
in response to the determination that the aircraft is on the desired path and while the aircraft is on the desired path, cause an action to be generated based on a comparison of the at least one predicted steering command with at least one current steering command and determine whether a range or threshold corresponding to the one or more actual operating characteristics is exceeded;
wherein the action is for assisting operation of the aircraft.
16. The system of claim 2 , wherein the signal is configured to cause an adjustment of a control parameter of the steering system.
17. The method of claim 14 , wherein the determining step includes determining if the condition of the aircraft is an abnormal condition and the signal causes adjustment of a control parameter applied to the steering.
18. A steering system for an aircraft comprising at least one controller configured to:
determine, based on one or more conditions, one or more expected operating characteristics of a steering system of the aircraft, the one or more expected operating characteristics being expected operating characteristics for controlling the aircraft on a surface to maintain the aircraft on a desired path along the surface, the one or more conditions comprising one or more aircraft conditions indicative of an internal condition of the aircraft and/or one or more external conditions indicative of an external influence on the aircraft;
provide an automated steering function to steer the aircraft along a desired path on a surface;
determine that the aircraft is on the desired path;
in response to determining that the aircraft is on the desired path and while the aircraft is on the desired path, determine one or more actual operating characteristics under which the steering system is being operated to control the steering of the aircraft on the desired path;
while the aircraft is on the desired path, perform a comparison process to compare the one or more expected operating characteristics with the one or more actual operating characteristics;
determine, based on the comparison, whether an allowable range or threshold corresponding to the one or more actual operating characteristics is exceeded;
determine, based on the determination of whether the allowable range or threshold is exceeded, a condition of the aircraft, and
depending on the condition, automatically disabling the automated steering function of the steering system.
19. The system according to claim 4 , further comprising, based on the comparison process, adjusting an allowable angular range of turning the nose wheel angle of the aircraft and/or the amount of rudder trim.