CN108170119A - A kind of front and rear cabin flight control system instruction integrated approach in combat trainer - Google Patents
A kind of front and rear cabin flight control system instruction integrated approach in combat trainer Download PDFInfo
- Publication number
- CN108170119A CN108170119A CN201711293218.0A CN201711293218A CN108170119A CN 108170119 A CN108170119 A CN 108170119A CN 201711293218 A CN201711293218 A CN 201711293218A CN 108170119 A CN108170119 A CN 108170119A
- Authority
- CN
- China
- Prior art keywords
- switch
- control
- override
- permission
- deck
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0259—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
- G05B23/0286—Modifications to the monitored process, e.g. stopping operation or adapting control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/12—Dual control apparatus
Abstract
The invention belongs to flight control system technology, the front and rear cabin flight control system instruction integrated approach being related in a kind of combat trainer.The present invention includes flying control override permission switch integrated logic, flies control override switch integrated logic, front and rear cabin control stick/pedal integrated logic and cockpit switch integrated logic.The present invention solves the problems, such as manipulation of the front and rear cabin without machinery crosslinking flight control system, improves flight control system safety, realizes front and rear cabin control command superposition under normal circumstances and switch order synthesis.
Description
Technical field
The invention belongs to flight control system technologies, are related to the front and rear cabin flight control system instruction synthesis side in a kind of combat trainer
Method.
Background technology
Cabin control stick/pedal component is generally using machinery crosslinking, cockpit control before and after conventional combat trainer flight control system
Switch generally uses hardware synthesis mode.Novel combat trainer is nervous in order to alleviate front and rear cockpit space, and flight control system uses
Completely self-contained control stick/pedal component and cockpit control switch；In order to improve system advance and realize more complicated
Control logic is widely used full powers limit, three axis, redundance fly-by-wire.
Since front and rear cockpit is without machinery crosslinking, flight control system must use strict digital command integrated logic, while real
Existing Training And Operations task, improves security of system.Flight control system by flight control computer realize system administration, redundancy management and
Control law calculates, and flight control computer is the core control component of full machine flight control system.
Invention content
The purpose of the present invention is：A kind of front and rear cabin flight control system instruction synthesis is provided for novel combat trainer flight control system
Method.
The technical scheme is that：A kind of front and rear cabin flight control system instruction integrated approach in combat trainer, including
Fly control override permission switch integrated logic, fly control override switch integrated logic, front and rear cabin control stick/pedal integrated logic and cockpit
Switch integrated logic；Wherein：
1st, fly control override permission switch integrated logic
" fly control override permission stacked switch " signal definition " 0 " is invalid for stacked switch, and " 1 " is front deck override permission, " 2 "
To shield rear deck permission, " 3 " are rear deck override permission.
Front deck is flown according to following logic to control override permission switch, shielding rear deck permission switch, rear deck override permission switch
Vote value is combined, and generates " flying control override permission stacked switch " signal, cabin control stick/pedal before and after being carried out using the signal
Instruction, cockpit switch integrated logic calculate；" flying control override permission stacked switch " signal generation logic is as follows：
1.a) if front deck, which flies to control override permission switch, shielding rear deck permission switch, rear deck override permission, switchs any one
The whole failures of switch put " flying control override permission stacked switch "=0, while light " front deck override permission " and " rear deck override power
Limit " indicator light exits " flying control override permission stacked switch " signal and calculates；
1.b) if front deck flies control override permission switch, shielding rear deck permission switchs, the switch appearance of rear deck override permission is following
" flying control override permission stacked switch "=0 is put in combination, at nonvolatile storage (Nonvolatile Memory, referred to as " NVM ")
Middle record flies control override permission stacked switch signal fault, while lights " front deck override permission " and " rear deck override permission " instruction
Lamp exits " flying control override permission stacked switch " signal and calculates：
I) any two be " 1 "；
II) three be " 1 "；
III) three be " 0 ".
If it is 1 that 1.c) front deck, which flies to control override permission switch, " flying control override permission stacked switch "=1 is put, is grasped as follows
Make：
I) if front deck flies control override switch, vote value is 0, light " front deck override permission " indicator light；
II) if front deck flies control override switch, vote value is 1, light " front deck override permission ", " control stick override " indicator light.
If 1.d) shielding rear deck permission switch is 1, " flying control override permission stacked switch "=2 are put, light " shielding rear deck power
Limit " indicator light；
If it is 1 that 1.e) rear deck, which flies to control override permission switch, " flying control override permission stacked switch "=3 are put, and carry out as follows
Operation：
I) if rear deck flies control override switch, vote value is 0, light " rear deck override permission " indicator light：
II) if rear deck flies control override switch, vote value is 1, light " rear deck override permission ", " control stick override " indicator light.
2nd, fly control override switch integrated logic
Combination, which is generated, according to lower row logic flies control override switch signal：
If 2.a) front and rear cabin switchs equal failure, combination vote value is failure safe value 0, puts control law reconstruction position, exits comprehensive
Logical calculating；
2.b) vote value is combined according to following algorithm to calculate：
Wherein：
V_vdfcsovdsw is the winged control override switch vote value after synthesis；
V_vdfcsovdsw_fwd flies to control override switch vote value for front deck；
V_vdfcsovdsw_aft flies to control override switch vote value for rear deck.
2.c) when front deck switch fault and rear deck switch fault-free：
I) if breaking down moment：When rear deck flies to control override switch connection, control law reconstruction position is not put；When rear deck flies to control
During override switch access failure, control law reconstruction position is put；
II) if after failure generation, rear deck flies to control override switch connection, removes control law reconstruction position.
2.d) when front deck switch fault-free, control law reconstruction position is not put.
3rd, front and rear cabin control stick/pedal integrated logic
For front and rear cabin control stick/pedal command signal, flight control system synthesis " flying control override permission stacked switch " and before
Rear deck flies to control override switch voting value signal, cabin control stick/pedal integrated logic before and after completion.Front and rear cabin control stick/pedal refers to
Enable integrated logic completely the same, integrated logic is as follows：
3.a) " fly control override permission stacked switch "=0
It is invalid to fly control override function at this time, control stick/pedal instruction send control according to result after forward and backward cabin instruction linear superposition
System rule calculates, and superposition logic is as follows：
Wherein：
V_v is control stick/pedal instruction that control law is sent to calculate；
V_v_fwd instructs vote value for front deck control stick/pedal；
V_v_aft instructs vote value for rear deck control stick/pedal；
VmaxMaximum forward displacement is instructed for control stick/pedal；
VminFor control stick/maximum negative sense displacement of pedal instruction.
3.b) " fly control override permission stacked switch "=1
I) if it is 0 that front deck, which flies control override switch vote value, control stick/pedal instruction is according to 3.a) item superposition；
II) if it is 1, v_v=v_v_fwd that front deck, which flies control override switch vote value,.
3.c) " fly control override permission stacked switch "=2, v_v=v_v_fwd；
3.d) " fly control override permission stacked switch "=3
I) if it is 0 that rear deck, which flies control override switch vote value, control stick/pedal instruction is according to 3.a) item superposition；
II) if it is 1, v_v=v_v_aft that rear deck, which flies control override switch vote value,.
4th, cockpit switch integrated logic
There is the switch of identical function for front and rear cabin, flight control system synthesis " fly control override permission stacked switch " and
Front and rear cabin flies to control override switch voting value signal, completes switch override logic, override logic is as follows：
4.a) " fly control override permission stacked switch "=0
It is invalid to fly control override function at this time, switching vote value synthesis generation voting signal according to forward and backward cabin send control law meter
It calculates, integrated logic is as follows：
Wherein：
V_vdsw is the switch vote value after synthesis；
V_vdsw_fwd switchs vote value for front deck；
V_vdsw_aft switchs vote value for rear deck.
4.b) " fly control override permission stacked switch "=1
I) if front deck flies control override switch, vote value is 0, according to 4.a) item synthesis；
II) if it is 1, v_vdsw=v_vdsw_fwd that front deck, which flies control override switch vote value,.
4.c) " fly control override permission stacked switch "=2, v_vdsw=v_vdsw_fwd；
4.d) " fly control override permission stacked switch "=3
I) if it is 0 that rear deck, which flies control override switch vote value, it is integrated according to a) item；
II) if it is 1, v_vdsw=v_vdsw_aft that rear deck, which flies control override switch vote value,.
The beneficial effects of the invention are as follows：Front and rear cockpit is completely independent without the crosslinked novel combat trainer of machinery, is adopted
Integrated management can be carried out to front and rear cockpit flight control system signal, solve front and rear cabin without machinery crosslinking flight control system with the present invention
Manipulation problem improves flight control system safety, realizes front and rear cabin control command superposition under normal circumstances and switch order synthesis,
In the case of front deck or rear deck signal fault, front deck or rear deck operation error, there is provided front and rear cabin override logics, it is ensured that flies control
System manipulation is normal, while considers operational need, and there is provided rear deck signal shielding functions.It is international first the invention belongs to domestic initiation
Into with certain novelty, which has been successfully applied in aircraft.Present invention comprehensive utilization cockpit hardware resource, is adopted
With strict digital command synthesis and override logic, flight control computer Airborne Software is needed to realize, front and rear cabin flight control system instruction
Integrated software is resided in flight control computer CPU, running software period 15ms.
Description of the drawings
Fig. 1 is the schematic diagram of cabin flight control system instruction integrated approach before and after the present invention.
Specific embodiment
The specific embodiment of the present invention is described further below in conjunction with the accompanying drawings.
Referring to Fig. 1, flight control computer acquisition flies control override permission switch, front and rear cabin control stick/pedal instruction, front and rear cabin seat
After the switching signal of cabin, by simulation/discrete signal voting/policing algorithm, generate and fly control override permission switch vote value and state
Signal flies control override switch vote value, front and rear cabin control stick/pedal instruction vote value, front and rear cabin cockpit switch vote value, above-mentioned
Cabin flight control system instruction integrated approach generates control stick/pedal instruction integrated signal and the comprehensive letter of cockpit switch before and after signal is sent into
Number, and above-mentioned signal is sent into control law and is calculated, while control control stick LED Unit, inform pilot's current state.
Front and rear cabin flight control system instruction integrated approach in a kind of combat trainer of the present invention, is opened including flying control override permission
It closes integrated logic, fly control override switch integrated logic, front and rear cabin control stick/pedal integrated logic and cockpit switch integrated logic；
Wherein：
1st, fly control override permission switch integrated logic
" fly control override permission stacked switch " signal definition " 0 " is invalid for stacked switch, and " 1 " is front deck override permission, " 2 "
To shield rear deck permission, " 3 " are rear deck override permission.
Front deck is flown according to following logic to control override permission switch, shielding rear deck permission switch, rear deck override permission switch
Vote value is combined, and generates " flying control override permission stacked switch " signal, cabin control stick/pedal before and after being carried out using the signal
Instruction, cockpit switch integrated logic calculate；" flying control override permission stacked switch " signal generation logic is as follows：
1.a) if front deck, which flies to control override permission switch, shielding rear deck permission switch, rear deck override permission, switchs any one
The whole failures of switch put " flying control override permission stacked switch "=0, while light " front deck override permission " and " rear deck override power
Limit " indicator light exits " flying control override permission stacked switch " signal and calculates；
1.b) if front deck flies control override permission switch, shielding rear deck permission switchs, the switch appearance of rear deck override permission is following
" flying control override permission stacked switch "=0 is put in combination, at nonvolatile storage (Nonvolatile Memory, referred to as " NVM ")
Middle record flies control override permission stacked switch signal fault, while lights " front deck override permission " and " rear deck override permission " instruction
Lamp exits " flying control override permission stacked switch " signal and calculates：
I) any two be " 1 "；
II) three be " 1 "；
III) three be " 0 ".
If it is 1 that 1.c) front deck, which flies to control override permission switch, " flying control override permission stacked switch "=1 is put, is grasped as follows
Make：
I) if front deck flies control override switch, vote value is 0, light " front deck override permission " indicator light；
II) if front deck flies control override switch, vote value is 1, light " front deck override permission ", " control stick override " indicator light.
If 1.d) shielding rear deck permission switch is 1, " flying control override permission stacked switch "=2 are put, light " shielding rear deck power
Limit " indicator light；
If it is 1 that 1.e) rear deck, which flies to control override permission switch, " flying control override permission stacked switch "=3 are put, and carry out as follows
Operation：
I) if rear deck flies control override switch, vote value is 0, light " rear deck override permission " indicator light：
II) if rear deck flies control override switch, vote value is 1, light " rear deck override permission ", " control stick override " indicator light.
2nd, fly control override switch integrated logic
Combination, which is generated, according to lower row logic flies control override switch signal：
If 2.a) front and rear cabin switchs equal failure, combination vote value is failure safe value 0, puts control law reconstruction position, exits comprehensive
Logical calculating；
2.b) vote value is combined according to following algorithm to calculate：
Wherein：
V_vdfcsovdsw is the winged control override switch vote value after synthesis；
V_vdfcsovdsw_fwd flies to control override switch vote value for front deck；
V_vdfcsovdsw_aft flies to control override switch vote value for rear deck.
2.c) when front deck switch fault and rear deck switch fault-free：
I) if breaking down moment：When rear deck flies to control override switch connection, control law reconstruction position is not put；When rear deck flies to control
During override switch access failure, control law reconstruction position is put；
II) if after failure generation, rear deck flies to control override switch connection, removes control law reconstruction position.
2.d) when front deck switch fault-free, control law reconstruction position is not put.
3rd, front and rear cabin control stick/pedal integrated logic
For front and rear cabin control stick/pedal command signal, flight control system synthesis " flying control override permission stacked switch " and before
Rear deck flies to control override switch voting value signal, cabin control stick/pedal integrated logic before and after completion.Front and rear cabin control stick/pedal refers to
Enable integrated logic completely the same, integrated logic is as follows：
3.a) " fly control override permission stacked switch "=0
It is invalid to fly control override function at this time, control stick/pedal instruction send control according to result after forward and backward cabin instruction linear superposition
System rule calculates, and superposition logic is as follows：
Wherein：
V_v is control stick/pedal instruction that control law is sent to calculate；
V_v_fwd instructs vote value for front deck control stick/pedal；
V_v_aft instructs vote value for rear deck control stick/pedal；
VmaxMaximum forward displacement is instructed for control stick/pedal；
VminFor control stick/maximum negative sense displacement of pedal instruction.
3.b) " fly control override permission stacked switch "=1
I) if it is 0 that front deck, which flies control override switch vote value, control stick/pedal instruction is according to 3.a) item superposition；
II) if it is 1, v_v=v_v_fwd that front deck, which flies control override switch vote value,.
3.c) " fly control override permission stacked switch "=2, v_v=v_v_fwd；
3.d) " fly control override permission stacked switch "=3
I) if it is 0 that rear deck, which flies control override switch vote value, control stick/pedal instruction is according to 3.a) item superposition；
II) if it is 1, v_v=v_v_aft that rear deck, which flies control override switch vote value,.
4th, cockpit switch integrated logic
There is the switch of identical function for front and rear cabin, flight control system synthesis " fly control override permission stacked switch " and
Front and rear cabin flies to control override switch voting value signal, completes switch override logic, override logic is as follows：
4.a) " fly control override permission stacked switch "=0
It is invalid to fly control override function at this time, switching vote value synthesis generation voting signal according to forward and backward cabin send control law meter
It calculates, integrated logic is as follows：
Wherein：
V_vdsw is the switch vote value after synthesis；
V_vdsw_fwd switchs vote value for front deck；
V_vdsw_aft switchs vote value for rear deck.
4.b) " fly control override permission stacked switch "=1
I) if it is 0 that front deck, which flies control override switch vote value, it is integrated according to a) item；
II) if it is 1, v_vdsw=v_vdsw_fwd that front deck, which flies control override switch vote value,.
4.c) " fly control override permission stacked switch "=2, v_vdsw=v_vdsw_fwd；
4.d) " fly control override permission stacked switch "=3
I) if rear deck flies control override switch, vote value is 0, according to 4.a) item synthesis；
II) if it is 1, v_vdsw=v_vdsw_aft that rear deck, which flies control override switch vote value,.
Claims (1)
1. the front and rear cabin flight control system instruction integrated approach in a kind of combat trainer is patrolled including flying control override permission switch synthesis
It collects, fly control override switch integrated logic, front and rear cabin control stick/pedal integrated logic and cockpit switch integrated logic；Wherein：
1) fly control override permission switch integrated logic
" flying control override permission stacked switch " signal definition " 0 " is invalid for stacked switch, and " 1 " is front deck override permission, and " 2 " are screen
Rear deck permission is covered, " 3 " are rear deck override permission；
Front deck is flown according to following logic to control override permission switch, shielding rear deck permission switch, the switch voting of rear deck override permission
Value is combined, and generates " flying control override permission stacked switch " signal, cabin control stick/pedal refers to before and after being carried out using the signal
It enables, cockpit switch integrated logic calculates；" flying control override permission stacked switch " signal generation logic is as follows：
1.a) if front deck, which flies to control override permission switch, shielding rear deck permission switch, rear deck override permission, switchs any one switch
Whole failures put " flying control override permission stacked switch "=0, while light " front deck override permission " and " rear deck override permission " and refer to
Show lamp, exit " flying control override permission stacked switch " signal and calculate；
If 1.b) front deck flies control override permission switch, shielding rear deck permission switchs, following combination occurs in rear deck override permission switch,
" flying control override permission stacked switch "=0 is put, is remembered in nonvolatile storage (Nonvolatile Memory, referred to as " NVM ")
Record flies control override permission stacked switch signal fault, while lights " front deck override permission " and " rear deck override permission " indicator light,
" flying control override permission stacked switch " signal is exited to calculate：
I) any two be " 1 "；
II) three be " 1 "；
III) three be " 0 "；
If it is 1 that 1.c) front deck, which flies to control override permission switch, " flying control override permission stacked switch "=1 is put, is proceeded as follows：
I) if front deck flies control override switch, vote value is 0, light " front deck override permission " indicator light；
II) if front deck flies control override switch, vote value is 1, light " front deck override permission ", " control stick override " indicator light；
If 1.d) shielding rear deck permission switch is 1, " flying control override permission stacked switch "=2 are put, are lighted " shielding rear deck permission "
Indicator light；
If it is 1 that 1.e) rear deck, which flies to control override permission switch, " flying control override permission stacked switch "=3 are put, and proceed as follows：
I) if rear deck flies control override switch, vote value is 0, light " rear deck override permission " indicator light：
II) if rear deck flies control override switch, vote value is 1, light " rear deck override permission ", " control stick override " indicator light；
2) fly control override switch integrated logic
Combination, which is generated, according to lower row logic flies control override switch signal：
If 2.a) front and rear cabin switchs equal failure, combination vote value is failure safe value 0, puts control law reconstruction position, exits synthesis and patrols
It collects and calculates；
2.b) vote value is combined according to following algorithm to calculate：
Wherein：
V_vdfcsovdsw is the winged control override switch vote value after synthesis；
V_vdfcsovdsw_fwd flies to control override switch vote value for front deck；
V_vdfcsovdsw_aft flies to control override switch vote value for rear deck；
2.c) when front deck switch fault and rear deck switch fault-free：
I) if breaking down moment：When rear deck flies to control override switch connection, control law reconstruction position is not put；When rear deck flies to control override
When switching access failure, control law reconstruction position is put；
II) if after failure generation, rear deck flies to control override switch connection, removes control law reconstruction position；
2.d) when front deck switch fault-free, control law reconstruction position is not put；
3) cabin control stick/pedal integrated logic before and after
For front and rear cabin control stick/pedal command signal, flight control system synthesis " flying control override permission stacked switch " and front and rear cabin
Fly control override switch voting value signal, cabin control stick/pedal integrated logic before and after completion；Front and rear cabin control stick/pedal instruction is comprehensive
Logical completely the same, integrated logic is as follows：
3.a) " fly control override permission stacked switch "=0
It is invalid to fly control override function at this time, control stick/pedal instruction send control law according to result after forward and backward cabin instruction linear superposition
It calculates, superposition logic is as follows：
Wherein：
V_v is control stick/pedal instruction that control law is sent to calculate；
V_v_fwd instructs vote value for front deck control stick/pedal；
V_v_aft instructs vote value for rear deck control stick/pedal；
VmaxMaximum forward displacement is instructed for control stick/pedal；
VminFor control stick/maximum negative sense displacement of pedal instruction；
3.b) " fly control override permission stacked switch "=1
I) if it is 0 that front deck, which flies control override switch vote value, control stick/pedal instruction is according to 3.a) item superposition；
II) if it is 1, v_v=v_v_fwd that front deck, which flies control override switch vote value,；
3.c) " fly control override permission stacked switch "=2, v_v=v_v_fwd；
3.d) " fly control override permission stacked switch "=3
I) if it is 0 that rear deck, which flies control override switch vote value, control stick/pedal instruction is according to 3.a) item superposition；
II) if it is 1, v_v=v_v_aft that rear deck, which flies control override switch vote value,；
4) cockpit switch integrated logic
There is the switch of identical function for front and rear cabin, flight control system integrates " flying control override permission stacked switch " and front and rear
Cabin flies to control override switch voting value signal, completes switch override logic, override logic is as follows：
4.a) " fly control override permission stacked switch "=0
It is invalid to fly control override function at this time, switching vote value synthesis generation voting signal according to forward and backward cabin send control law to calculate, comprehensive
It is logical as follows：
Wherein：
V_vdsw is the switch vote value after synthesis；
V_vdsw_fwd switchs vote value for front deck；
V_vdsw_aft switchs vote value for rear deck；
4.b) " fly control override permission stacked switch "=1
I) if front deck flies control override switch, vote value is 0, according to 4.a) item synthesis；
II) if it is 1, v_vdsw=v_vdsw_fwd that front deck, which flies control override switch vote value,；
4.c) " fly control override permission stacked switch "=2, v_vdsw=v_vdsw_fwd；
4.d) " fly control override permission stacked switch "=3
I) if it is 0 that rear deck, which flies control override switch vote value, it is integrated according to a) item；
II) if it is 1, v_vdsw=v_vdsw_aft that rear deck, which flies control override switch vote value,.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711293218.0A CN108170119B (en) | 2017-12-08 | 2017-12-08 | Instruction integration method for flight control system of front cabin and rear cabin in combat trainer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711293218.0A CN108170119B (en) | 2017-12-08 | 2017-12-08 | Instruction integration method for flight control system of front cabin and rear cabin in combat trainer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108170119A true CN108170119A (en) | 2018-06-15 |
| CN108170119B CN108170119B (en) | 2020-06-30 |
Family
ID=62525569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711293218.0A Active CN108170119B (en) | 2017-12-08 | 2017-12-08 | Instruction integration method for flight control system of front cabin and rear cabin in combat trainer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108170119B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112462800A (en) * | 2020-11-05 | 2021-03-09 | 哈尔滨飞机工业集团有限责任公司 | Hovering rear cabin control method for search and rescue type helicopter |
| CN114435604A (en) * | 2021-12-15 | 2022-05-06 | 中国航空工业集团公司成都飞机设计研究所 | High-safety throttle permission switching and instruction comprehensive control method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2216245A1 (en) * | 2009-02-10 | 2010-08-11 | Airbus Operations | Flight-control system and aircraft comprising same |
| CN204623824U (en) * | 2015-05-05 | 2015-09-09 | 江西洪都航空工业集团有限责任公司 | A kind of flight control system |
| CN106628123A (en) * | 2016-12-28 | 2017-05-10 | 中国航空工业集团公司西安飞机设计研究所 | Distributed airplane flap control system |
-
2017
- 2017-12-08 CN CN201711293218.0A patent/CN108170119B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2216245A1 (en) * | 2009-02-10 | 2010-08-11 | Airbus Operations | Flight-control system and aircraft comprising same |
| US20100222943A1 (en) * | 2009-02-10 | 2010-09-02 | Airbus Operations (S.A.S.) | Flight control system and aircraft comprising it |
| CN204623824U (en) * | 2015-05-05 | 2015-09-09 | 江西洪都航空工业集团有限责任公司 | A kind of flight control system |
| CN106628123A (en) * | 2016-12-28 | 2017-05-10 | 中国航空工业集团公司西安飞机设计研究所 | Distributed airplane flap control system |
Non-Patent Citations (1)
| Title |
|---|
| 唐志帅 等: "民用飞机飞控系统传感器信号表决设计", 《民用飞机设计与研究》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112462800A (en) * | 2020-11-05 | 2021-03-09 | 哈尔滨飞机工业集团有限责任公司 | Hovering rear cabin control method for search and rescue type helicopter |
| CN114435604A (en) * | 2021-12-15 | 2022-05-06 | 中国航空工业集团公司成都飞机设计研究所 | High-safety throttle permission switching and instruction comprehensive control method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108170119B (en) | 2020-06-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11592841B2 (en) | In-flight stabilization of an aircraft | |
| CN102571741B (en) | Safety " client-server " computer system for interactive application | |
| US20210371123A1 (en) | In-flight stabilization of an aircraft | |
| US20140005862A1 (en) | Method and Apparatus for Aircraft Sensor and Actuator Failure Protection Using Reconfigurable Flight Control Laws | |
| CN108170119A (en) | A kind of front and rear cabin flight control system instruction integrated approach in combat trainer | |
| US20210380224A1 (en) | In-flight stabilization of an aircraft | |
| KR20030004310A (en) | Multi-mode tiltrotor nacelle control system with integrated envelope protection | |
| RU2014132221A (en) | CENTRIFUGE-BASED TRAINING SIMULATOR | |
| CN110930812A (en) | Control system for airplane simulation cockpit | |
| US20210339882A1 (en) | In-flight stabilization of an aircraft | |
| CN104536455B (en) | Flight control method of unmanned general aircraft with flight experience function | |
| CN111874256A (en) | Fault emergency processing method and device for solar unmanned aerial vehicle | |
| US20230312085A1 (en) | Method and system for fly-by-wire flight control configured for use in electric aircraft | |
| CN113534656B (en) | Telex flight backup control system and telex flight backup control method | |
| CN105292503B (en) | A kind of safe and efficient automatic flight control system control indication mechanism | |
| CN111564083A (en) | Aircraft aerodynamic physical simulation system | |
| CN103466102A (en) | Spacecraft control action redistribution method on condition of cross configuration actuating mechanism in fault | |
| US20100030402A1 (en) | Light multi-purpose aircraft with a controlling integrated complex | |
| US11393355B1 (en) | System for flight simulation of an electric aircraft | |
| CN106828884A (en) | The method that amphibious aircraft flight control system installs control augmentation stability system additional | |
| US20240067352A1 (en) | Methods and system for estimating percentage torque produced by a propulsor configured for use in an electric aircraft | |
| Papathakis et al. | Safety considerations for electric, hybrid-electric, and turbo-electric distributed propulsion aircraft testbeds | |
| US20230219692A1 (en) | High voltage distribution systems and methods | |
| US20230144771A1 (en) | Systems and methods for simulating an electrical vertical takeoff and landing (evtol) aircraft | |
| CN110803290B (en) | Novel ejection seat program control method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |