Aircraft control mode transition smoothing
US-2019155282-A1 · May 23, 2019 · US
US11059568B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11059568-B2 |
| Application number | US-201916298480-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 11, 2019 |
| Priority date | Mar 11, 2019 |
| Publication date | Jul 13, 2021 |
| Grant date | Jul 13, 2021 |
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A control system having a variable operator interface (VOI) is disclosed, and includes one or more processors and a memory coupled to the processors. The memory stores program code causing the control system to detect an existence and first direction of an operator control input to one or more active inceptors being backdriven from an operator on inceptor detector (OID). The control system is caused to compare the first direction of the operator control input with a second direction of one or more zero-force detent rates to determine a variance and interprets the operator control input as inadvertent based on the variance. In response to interpreting the operator control input as inadvertent, the control system is caused to limit the operator control input to reduce or substantially eliminate movement of the machine caused by inadvertent input by modifying the operator control input based on one or more command modifiers.
Opening claim text (preview).
What is claimed is: 1. A control system ( 54 ) for a machine ( 10 ) having a variable operator interface (VOI) ( 55 ), the control system ( 54 ) comprising: one or more processors ( 84 ); and a memory ( 82 ) coupled to the one or more processors ( 84 ), the memory ( 82 ) storing program code that, when executed by the one or more processors ( 84 ), causes the control system ( 54 ) to: detect an existence and a first direction of an operator control input ( 62 ) to one or more active inceptors ( 14 ) being backdriven from an operator on inceptor detector (OID) ( 94 ); compare the first direction of the operator control input ( 62 ) with a second direction of one or more zero-force detent rates (D) to determine a variance; interpret the operator control input ( 62 ) as inadvertent based on the variance between the first direction and the second direction; and in response to interpreting the operator control input ( 62 ) as inadvertent, limit the operator control input ( 62 ) to reduce or substantially eliminate movement of the machine ( 10 ) caused by inadvertent input by modifying the operator control input ( 62 ) based on one or more command modifiers. 2. The control system ( 54 ) of claim 1 , wherein the one or more processors ( 84 ) execute instructions to: determine a variable inceptor command deadzone (VICD) ( 96 ), wherein the VICD ( 96 ) is one of the one or more command modifiers; and apply the (VICD) ( 96 ) to an input of a command model ( 88 ). 3. The control system ( 54 ) of claim 2 , wherein the one or more processors ( 84 ) determine the VICD ( 96 ) by executing instructions to: determine the one or more zero-force detent rates (D) is above a predetermined threshold ( 114 ) of the zero-force detent rates (D); calculate a VICD size (E) based on the one or more zero-force detent rates (D) above the predetermined threshold ( 114 ) of the zero-force detent rates (D); and smooth the VICD ( 96 ) by applying one or more of low-pass filtering and time delays to the VICD ( 96 ); and reduce or substantially eliminate rapid changes in the VICD size (E) as the one or more zero-force detent rates (D) return below the predetermined threshold ( 114 ) of the zero-force detent rates (D). 4. The control system ( 54 ) of claim 2 , wherein a force feel profile ( 79 ) is linear within a detent width ( 97 ) and a detent force gradient ( 80 ) decreases outside the detent width ( 97 ). 5. The control system ( 54 ) of claim 2 , further comprising: apply a detent rate limiter (DRL) ( 100 ) to the one or more zero-force detent rates (D), wherein the DRL ( 100 ) is one of the one or more command modifiers. 6. The control system ( 54 ) of claim 5 , wherein the one or more zero-force detent rates (D) is a commanded rate of movement of a zero-force detent ( 51 ) of the one or more active inceptors ( 14 ), and wherein the one or more processors ( 84 ) executes instructions to: calculate the one or more zero-force detent rates (D) from an off-axis detent rate command from decoupling ( 108 ) and machine states to the one or more active inceptors ( 14 ); and compute an overall detent rate in an on-axis direction by using off-axis operator control inputs in combination with a current machine state ( 33 ) as input. 7. The control system ( 54 ) of claim 5 , wherein the one or more zero-force detent rates (D) is a function of a current machine state ( 33 ) and the first direction of the operator control input ( 62 ) to the one or more active inceptors ( 14 ). 8. The control system ( 54 ) of claim 5 , wherein the one or more processors ( 84 ) determine a variable asymmetric breakout force (VABF) ( 98 ) that is one of the one or more command modifiers by executing instructions to: modify a force feel profile ( 79 ) generated by a force feel generator ( 122 ) operably connected to the one or more active inceptors ( 14 ) by: adjust a breakout force F BO generated by the force feel generator ( 122 ) of the one or more active inceptors ( 14 ) along a detent force gradient ( 80 ) proportional to the one or more zero-force detent rates (D). 9. The control system ( 54 ) of claim 8 , wherein the one or more processors ( 84 ) adjust the breakout force F BO by executing instructions to: modify a breakout force F BO position to follow VICD ( 96 ) boundaries ( 116 ); and set the breakout force F BO as proportional to the one or more zero-force detent rates (D). 10. The control system ( 54 ) of claim 8 , further comprising one or more inline actuators ( 32 ) operably connected to the one or more active inceptors ( 14 ) of the VOI ( 55 ), wherein the one or more processors ( 84 ) adjust the breakout force F BO by executing instructions to: increase the breakout force F BO when a direction of the operator control input ( 62 ) is opposite to a direction of the one or more zero-force detent rates (D) as determined by the OID ( 94 ), and wherein the DRL ( 100 ) applies a rate limit to a commanded zero-force detent ( 51 ), and wherein the one or more processors ( 84 ) reduce or substantially eliminate movement of the machine ( 10 ) by executing instructions to reduce or substantially eliminate movement of the machine ( 10 ) via one or more control effector devices ( 18 ) and the one or more inline actuators ( 32 ). 11. The control system ( 54 ) of claim 1 , further comprising one or more inline actuators ( 32 ) operably connected to the one or more active inceptors ( 14 ) of the VOI ( 55 ), wherein the one or more processors ( 84 ) executes instructions to: detect the operator control input ( 62 ) to the one or more active inceptors ( 14 ) through the OID ( 94 ), wherein the control system ( 54 ) reduces or substantially eliminates movement of the machine ( 10 ) by controlling movement of the one or more inline actuators ( 32 ). 12. A method for limiting operator control input ( 62 ) in a machine ( 10 ), wherein the machine ( 10 ) includes a control system ( 54 ) having a variable operator interface (VOI) ( 55 ), the method comprising: detecting, by a control module ( 20 ), an existence and a first direction of the operator control input ( 62 ) to one or more active inceptors ( 14 ) being backdriven from an operator on inceptor detector (OID) ( 94 ); comparing the first direction of the operator control input ( 62 ) with a second direction of one or more zero-force detent rates (D) to determine a variance; interpreting the operator control input ( 62 ) as inadvertent based on the variance between the first direction and the second direction; and in response to interpreting the operator control input ( 62 ) as inadvertent, limiting the operator control input ( 62 ) to reduce or substantially eliminate movement of the machine ( 10 ) caused by inadvertent input by modifying the operator control input ( 62 ) based on one or more command modifiers. 13. The method of claim 12 , wherein the method further comprises: determining a variable inceptor command deadzone (VICD) ( 96 ), wherein the VICD ( 96 ) is one of the one or more command modifiers; and applying the (VICD) ( 96 ) to an input of a command model ( 88 ). 14. The method of claim 13 , wherein the method further comprises: determining the one or more zero-force detent rates (D) is above a predetermined threshold ( 114 ) of the zero-force detent rates (D); calculating a VICD size (E) based on the one or more zero-force detent rates (D) above the predetermined threshold ( 114 ) of the zero-force detent rates (D); smoothening the VICD ( 96 ) by applying one or more of low-pass filtering and time delays to the VICD ( 96 ); and reducing or substantially eliminating rapid changes in the VICD
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