CN117198116A - Coriolis flight illusion simulation method - Google Patents

Abstract

The application discloses a Coriolis flight illusion simulation method, which is used for a flight illusion simulator; the method comprises the following steps: receiving the setting operation of flight parameters by training personnel, and generating a target flight task; the method comprises the steps of sending first flight indication information to trained personnel, so that the trained personnel can finish take-off operation under the indication of the first flight indication information and keep flying flatly after reaching a preset height; sending second flight indication information to the trained personnel so that the trained personnel enter a horizontal continuous turn in a flat flight stage under the indication of the second flight indication information; sending third flight indication information to the trained personnel so that the trained personnel generates Coriolis Li Cuojiao in the process of moving the head; and sending fourth flight indication information to the trained personnel so as to enable the trained personnel to gradually eliminate the Coriolis illusion. By utilizing the scheme of the application, the pilot can be helped to recognize, identify and correctly handle the illusion of flight, so that the accident rate is effectively reduced.

Description

Coriolis flight illusion simulation method

Technical Field

The application relates to the technical field of flight simulation, in particular to a Coriolis flight illusion simulation method.

Background

The illusion of flight, also known as a spatial orientation disorder, is the incorrect perception of the position, attitude, direction and movement of the aircraft or itself by the pilot while in flight. The illusion of flight is one of the most important factors in serious flight accidents related to human factors, and is common among flight personnel, so that the flight efficiency of pilots is influenced, and the flight safety is compromised. In general, the human body mainly relies on its own vision, vestibular sensation, proprioception to perform spatial orientation, and determines its own state and position. When a pilot flies in the air, the human body has a certain limitation on six-freedom complex motions in the air and limited visual scene conditions due to the physiological functions of the human body's own sense organs and the central nervous system motion perception modes, so that the occurrence of the illusion of flying can be caused. Complex weather such as cloud, fog, rain, snow and the like encountered in flight, linear acceleration and angular velocity stimulation in flight, night flight, offshore flight and the like are all important factors for inducing the illusion of flight.

The coriolis illusion (Coriolis illusion) is an illusion of vestibular flight, which means that when the pilot turns the pilot about a certain axis (vertical, pitch or roll axis) while the pilot is flying, if the head is simultaneously rotating about a second axis, the pilot experiences an illusion of turning about a third axis due to coriolis acceleration. The coriolis illusion is an illusion of flight with a high incidence and a high hazard. In actual flight, when the aircraft is in a maneuvering flight process such as hovering, rolling or fighting, the pilot simultaneously performs head movements such as head lowering, head swinging and the like, and the illusion is extremely easy to induce. When the Coriolis illusion occurs, on one hand, the pilot can generate strong discomforts such as dizziness, nausea, cold sweat, even vomiting and the like, and the manipulation and cognitive ability of the pilot are reduced; on the other hand, coriolis acceleration causes the vestibular organ of the pilot to generate an actually nonexistent false sense of rotation around the third axis, and at this time, the aircraft is extremely easy to run away or enter a complex state due to incorrect corrective maneuvering actions of the pilot, so that a flight accident occurs.

In the related art, the scheme for overcoming the coriolis illusion is generally a conventional method for effectively performing spatial orientation and overcoming the illusion of flight according to the visual instrument flight. The pilot can effectively overcome the illusion of flying by depending on reliable and correct directional information sources, such as flying according to instruments, and the occurrence of flying accidents is avoided. However, on one hand, the instrument visual space orientation has the problems of indirection, instability and the like, and if the instrument flight technique is not skilled, the coriolis flight illusion cannot be recognized and identified, and the instrument visual space orientation is difficult to play an effective role; on the other hand, the coriolis illusion can make the pilot produce real and strong motor feeling, under the condition of collision of instruments and feeling, if the coriolis illusion is not trained, the instinct of the pilot can more easily trust the sense of the pilot, and further the illusion occurs to cause the flying accident, so that a flying illusion simulation method is needed to be provided to develop the coriolis illusion experience training on the flying illusion simulator, help the pilot to recognize, identify and correctly treat the flying illusion, and effectively reduce the accident rate.

Disclosure of Invention

The application provides a Coriolis illusion flight simulation method, which is used for developing Coriolis illusion flight experience training on an illusion flight simulator and helping pilots to recognize, identify and correctly treat illusions of flight so as to effectively reduce accident rate.

Therefore, the application provides the following technical scheme:

a Coriolis flight illusion simulation method is used for a flight illusion simulator; the method comprises the following steps:

receiving the setting operation of flight parameters by training personnel, and generating a target flight task;

sending first flight indication information to a trained person, so that the trained person finishes take-off operation according to information displayed by an instrument display system under the indication of the first flight indication information and keeps flying flatly after reaching a preset height;

sending second flight indication information to the trained personnel, so that the trained personnel enters a horizontal continuous turn in a flat flight stage according to information displayed by an instrument display system under the indication of the second flight indication information;

sending third flight indication information to the trained personnel so that the trained personnel generates Coriolis Li Cuojiao in the process of moving the head;

and sending fourth flight indication information to the trained personnel so as to enable the trained personnel to gradually eliminate the Coriolis illusion.

Optionally, the target flight mission is a complex meteorological flight under diurnal preset meteorological parameters.

Optionally, the preset complex weather condition includes any one of the following: flying in the cloud, flying on the cloud with cloud cover of more than 80 percent, and flying under the cloud with visibility of less than 5 km.

Optionally, the target flight task includes: daytime complex meteorological flight tasks.

Optionally, the preset height is greater than the cloud layer height.

Optionally, the trained personnel entering a horizontal continuous turn in a flat flight phase according to the information displayed by the instrument display system under the indication of the second flight indication information includes: the trained personnel rolls rapidly to the right or left to the maximum grade with an angular acceleration above the human perception threshold and maintains the altitude.

Optionally, the flight simulator comprises: simulating a cabin, a six-degree-of-freedom motion platform and a 360-degree continuous rotation platform;

the trained personnel entering a horizontal continuous turn in a flat flight stage according to the information displayed by the instrument display system under the indication of the second flight indication information further comprises: and controlling the six-degree-of-freedom motion platform to drive the simulation cabin to roll to the right or left for inclination by a set angle, and simultaneously controlling the 360-degree continuous rotation platform to drive the simulation cabin to slowly accelerate to the right or left to a set angular speed at an angular acceleration below the human body feeling threshold value, and then continuously rotating at a constant speed.

Optionally, the third flight indication information is used for indicating the trained personnel to quickly perform head movements.

Optionally, the head action includes any one or more of: low head, head up, head swing right, head swing left.

Optionally, the fourth indication is used for indicating the trained personnel to restore the upright position of the head, and the instrument parameters are credited, so that the turning flight is kept.

According to the Coriolis flight illusion simulation method provided by the application, the Coriolis acceleration is generated to stimulate the vestibular sense organ of the pilot by setting the flight subjects and complex meteorological conditions and controlling 360-degree continuous rotation platform movement according to the spiral flight attitude by using the flight illusion simulator, so that the pilot experiences and correctly recognizes the Coriolis flight illusion in the process of executing the simulated flight task, the Coriolis flight illusion feeling is strong, the simulation effect is lifelike and stable, and the success rate is high.

Drawings

FIG. 1 is a schematic diagram of a flight illusion simulator used in the method of the present application;

fig. 2 is a flow chart of a coriolis illusion simulation method provided by the present application.

Detailed Description

In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings that are required to be used in the embodiments will be briefly described below. It is apparent that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained from these drawings without inventive effort for a person of ordinary skill in the art.

In describing embodiments of the present application, the terms "longitudinal," "transverse," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in terms of orientation or positional relationship shown in the drawings for convenience of description and simplicity of description only, and do not denote or imply that the devices or elements in question must have a particular orientation, be constructed and operated in a particular orientation, so that the above terms are not to be construed as limiting the application.

The present application will be described in detail below with reference to the drawings and the specific embodiments, which are not described in detail herein, but the embodiments of the present application are not limited to the following embodiments.

Aiming at the damage caused by the Coriolis illusion, the embodiment of the application provides a Coriolis illusion simulation method, which utilizes an illusion simulator to generate Coriolis acceleration to stimulate the vestibular sensing organ of a pilot by setting a flight subject and complex meteorological conditions and controlling 360-degree continuous rotation platform movement according to the spiral flight attitude, so that the pilot experiences and correctly recognizes the Coriolis illusion in the process of executing a simulated flight task, thereby helping the pilot to recognize, recognize and correctly treat the illusion and effectively reducing the probability of flight accidents.

The following first briefly describes a flight illusion simulator used in the coriolis flight illusion simulation method of the present application.

Fig. 1 is a schematic diagram of a schematic configuration of a coriolis illusion simulator used in the coriolis illusion simulation method of the present application.

The illusion simulator 100 includes: a simulation pod 101, a six degree of freedom motion platform 102, a 360 degree continuous rotation platform 103, a simulation system 104, and a supervisory control system 105. Wherein:

the simulation cabin 101 is used for carrying trained personnel and is driven by the six-degree-of-freedom motion platform 102 and the 360-degree continuous rotation platform 103 to move. The simulation cabin 101 comprises a control system 111, a view display system 112 and an instrument display system 113, wherein the control system 111 comprises a control steering rod, a foot rudder and a throttle, the instrument display system 113 comprises a head-up display and a horizon instrument, and the view display system 112 comprises an outdoor view display.

The 360-degree continuously rotating platform 103 may be fixedly installed on the upper portion of the six-degree-of-freedom motion platform 102 or the lower portion of the six-degree-of-freedom motion platform 102. The simulation cabin 101 fixed on the platform is driven, or the six-degree-of-freedom motion platform 102 and the simulation cabin 101 fixed on the platform are driven to continuously rotate around a vertical axis by +/-360 degrees.

The simulation cabin 101 is fixedly installed on the 360-degree continuous rotation platform 103 or the six-degree-of-freedom motion platform 102. A view display system 112, an instrument display system 113 and a manipulation system 111 are arranged in the simulation cabin 101, wherein the view display system 112 is used for providing a flight simulation view, and the instrument display system 113 comprises a horizon instrument, a head-up display and a liquid crystal instrument panel for displaying a flight instrument. The maneuvering system 111 is configured to receive flight maneuvering instructions from a trainee.

The simulation system 104 is configured to collect a trainee manipulation instruction signal, calculate, in real time, a flight parameter of the simulator 100 according to the collected trainee manipulation instruction signal, a state of the flight illusion simulator 100, and environmental information, and combine a preset flight model, and send the flight parameter to the six-degree-of-freedom motion platform 102, the vision display system 112, and the instrument display system 113 in real time, so as to feed back, to the trainee, the flight state under the current operation instruction in real time.

The management control system 105 includes an interaction module, a control module, and a monitoring storage module. The interaction module is used for receiving selection operation of trained personnel on the flight mode and the flight parameters; the control module is used for executing the step of the Coriolis flight illusion simulation method provided by the application; the monitoring storage module is used for collecting, monitoring and storing the physiological behavior states of trained personnel and the states of the running parameters of various systems such as a motion platform, flight simulation and the like.

In one non-limiting embodiment, the six degree of freedom motion stage 102 may include a spatial parallel motion mechanism including a lower stationary stage, an upper motion stage, 6 servo rams, a universal hinge joint, a travel limit mechanism.

By controlling the servo motor to change the length of the actuator cylinder, the attitude change of the cabin can be simulated at the upper part of the six-degree-of-freedom motion platform, and the pitching, rolling and yawing angular motions around three spatial coordinate axes and the lifting, traversing and longitudinally moving linear motions along three axes are realized. After receiving the aircraft motion parameters such as the real-time speed and acceleration of the aircraft of the simulation system 104, the control module of the six-degree-of-freedom motion system converts the aircraft motion parameters into the motion parameters of the platform, and controls the six-degree-of-freedom motion platform 102 to provide overload feeling and dynamic information of change of attitude angles in a certain range for trained personnel in the simulation cabin 101, so that the flight personnel generate motion feeling consistent with the actual flight environment and task conditions.

The six-degree-of-freedom motion platform 102 has a motion washing function, and the motion washing function characterizes a motion process that the six-degree-of-freedom motion platform 102 can return to a neutral position in a gentle motion lower than a human vestibular sensation threshold after completing one burst motion, so that the six-degree-of-freedom motion platform 102 can execute a next burst motion instruction within a preset displacement stroke range.

Illustratively, the vision display system 112 may include a display subsystem, a vision generation subsystem, and a scene database, which may provide a realistic, stable, real-time, exterior simulated view of the aircraft cabin for the pilot to determine the attitude, position, weather conditions, ground and airborne targets, etc. of the aircraft. Wherein, the display subsystem can adopt projection display or liquid crystal display technology; the vision generation subsystem can generate complex meteorological conditions such as topography, cloud, rain, fog and the like and images such as three-dimensional objects and the like in real time based on a high-performance graphic workstation and vision simulation software, so as to complete scene management; the scene database provides a geographical database such as plain, forest, ocean and the like and a three-dimensional object database of an airplane, an airport and a building;

the manipulation system 111 may include: steering column, rudder, throttle. The primary function of the control system 111 is to provide control command inputs for flight simulation in response to flight crew control commands.

The instrument display system 113 is used to simulate various flight instruments and heads-up displays in the aircraft cabin, the flight instruments being displayed on a central instrument liquid crystal panel, and the heads-up display being displayed in the central field of view of the vision display subsystem. The appearance of the meter and the index characteristics in the simulation range are consistent with the model to be simulated. The flight instrument of the central instrument panel mainly comprises a horizon instrument, an airspeed meter, an altimeter, a compass and the like; ping Xian can indicate the heading, lifting speed, airspeed, altitude, pitch angle, tilt angle, etc.

In the illusion simulator 100, the simulation system 104 collects pilot manipulation command signals, aircraft state and environmental information in real time, and calculates flight parameters such as aircraft speed, acceleration, euler angles and the like according to an aircraft aerodynamic model, a quality characteristic model and an engine model. The simulation system 104 sends the flight parameters to the six-degree-of-freedom motion platform 102, the visual display system 112 and the instrument display system 113 in real time, and feeds back the flight state to the pilot in real time.

In the flight illusion simulator 100, the management control system 105 is a main interface of the flight illusion simulator 100, and can provide function options and parameter settings for training personnel, control implementation of a flight illusion simulation method, and realize collection, monitoring and storage of running parameter states of each system and physiological behavior state information of the trained personnel.

The embodiment of the application provides a Coriolis flight illusion simulation method, which is used for the above-mentioned flight illusion simulator, and by setting flight subjects and complex meteorological conditions and controlling 360-degree continuous rotation platform movement according to spiral flight attitude, coriolis acceleration is generated to stimulate pilot vestibular sensing organs, so that pilot experiences and correctly identifies Coriolis flight illusions in the process of executing simulated flight tasks

As shown in fig. 2, a flow chart of the coriolis illusion simulation method provided by the application includes the following steps:

step 201, receiving a setting operation of flight parameters by a training person, and generating a target flight task.

The target flight mission may include, but is not limited to: daytime complex meteorological flight tasks. The preset complex weather conditions may include, for example, but are not limited to, any of the following: in-cloud flight, over-cloud flight with cloud cover >80%, under-cloud flight with visibility <5km, etc.

Referring also to fig. 1, illustratively, the trainee may implement an input operation of the flight parameters through an interaction module in the management system 105 in the flight illusion simulator 100, and the flight illusion simulator 100 generates a target flight mission according to the received setting operation of the flight parameters. The preset meteorological parameters corresponding to the target flight mission are set in the flight illusion simulator 100 as visibility of 3km, cloud cover of 10 (namely sky is full of clouds), and cloud base height of 2000 meters and Yun Hou-3000 meters. The target flight mission may be selected as a complex weather flight mission and the time may be selected as daytime. The aircraft type, airport territory, etc. may be selected by themselves based on configuration options associated with the illusion simulator 100, which is not limiting in this embodiment of the application.

By setting the target flight task in the mode, when a pilot flies, the pilot cannot see the landmark, the ground line which is referred by the visual space orientation is disappeared, the outside view cannot provide a movement clue, the pilot can generate space orientation difficulty, and then the vestibular illusion is easily induced under the condition that the pilot relies on the vestibular sensory system to orient more.

And 202, sending first flight indication information to trained personnel, so that the trained personnel can finish take-off operation according to information displayed by an instrument display system under the indication of the first flight indication information and keep flying flatly after reaching a preset height.

The predetermined height is greater than the cloud height, for example, the predetermined height is preferably greater than 3000 meters.

And 203, sending second flight indication information to the trained personnel, so that the trained personnel can enter a horizontal continuous turn in a flat flight stage according to the information displayed by the instrument display system under the indication of the second flight indication information.

The trained personnel enter a horizontal continuous turn in a flat flight stage and can roll to the maximum gradient of 30 degrees to the right or left rapidly with the angular acceleration above the human body feel threshold value, and the altitude is kept.

Specifically, referring to fig. 1, the six-degree-of-freedom motion platform 102 may be controlled to drive the simulation cabin 101 to roll to the right or left by a set angle, and at the same time, the 360-degree continuous rotation platform 103 is controlled to drive the simulation cabin 101 to slowly accelerate to the right or left to a set angular velocity with an angular acceleration below the human body feeling threshold, and then continuously rotate at a constant speed.

Illustratively, after the aircraft has completed the takeoff phase and is on a flat fly at a predetermined altitude, the trained personnel feel a threshold value (e.g., the threshold value is 0.5 °/s) ² ) The above angular acceleration rapidly rolls to the right (or left) to the maximum gradient of 30 deg., maintaining the altitude. In the process, the six-degree-of-freedom motion platform 102 in fig. 1 is controlled to drive the simulation cabin 101 to roll and tilt by 10 degrees to the right (or to the left), and meanwhile, the 360-degree continuous rotation platform 103 is controlled to drive the simulation cabin 101 to slowly accelerate to the right (or to the left) to 30 degrees/s at an angular acceleration below the human body sensory threshold, and then the simulation cabin continuously rotates at a constant speed. At this time, the trained personnel in the cockpit will feel the instantaneous angular acceleration of the aircraft rolling to the right (or left) and will not feel the continuous rotation to the right (or left) about the vertical axis, consistent with the actual flight experience.

And step 204, sending third flight indication information to the trained personnel so as to enable the trained personnel to generate Coriolis illusion in the process of moving the head.

The third flight indication information is used for indicating the trained personnel to quickly perform head movements, and the head movements can include, but are not limited to, any one or more of the following: low head, head up, head swing to the right, head swing to the left, etc.

Illustratively, the trained personnel is sent a low head (or head up) 30 ° view of the center dashboard (out-of-cabin view). Optionally, a 30 ° indication of the right (or left) lateral shoulder swing is sent to the trained person. Referring to fig. 1, in the process, the 360-degree continuous rotation platform 103 is controlled to drive the simulation cabin 101 to rotate at a constant speed of 30 °/s. At this time, the trainee's head is rapidly rotated about the second axis, i.e., the pitch axis, downward (or upward) or left (or right) about the roll axis while performing a rotational motion about the vertical axis at 30 °/s rightward (or leftward), and the trainee's head is subjected to coriolis acceleration, thereby stimulating the vestibular semicircular canal to generate a sense of rolling left (or right) about the third axis, i.e., the roll axis, or overturning upward (or downward) about the pitch axis. Because of the lack of visual orientation information outside the cockpit under complex weather conditions, pilots feel only against the vestibule, creating a stronger coriolis illusion of flight.

And step 205, sending fourth flight indication information to the trained personnel so as to enable the trained personnel to gradually eliminate the Coriolis illusion.

The fourth indication is used for indicating the trained personnel to restore the upright position of the head, and the instrument parameters are trusted to keep turning flight.

Illustratively, an instruction is given to the trainee to resume and maintain the upright position of the head indicating that the pilot is crediting the instrument parameters and continuing to maintain the continuous cornering flight for 60 seconds. Referring to fig. 1, in the process, the 360-degree continuous rotation platform 103 is controlled to drive the simulation cabin 101 to slowly decelerate to a stop at an angular acceleration below the human sensory threshold. At this point, the coriolis acceleration experienced by the trainee's head will disappear, and the perceived coriolis illusion, which turns left (or right) about the roll axis or up (or down) about the pitch axis, will diminish rapidly.

According to the Coriolis flight illusion simulation method provided by the application, through setting the flight subjects and the complex meteorological conditions and controlling the 360-degree continuous rotation platform to move according to the spiral flight attitude, the Coriolis acceleration is generated to stimulate the vestibular sensing organ of the pilot, so that the pilot experiences and correctly recognizes the Coriolis flight illusion in the process of executing the simulated flight task, the Coriolis flight illusion experience is strong, the simulation effect is lifelike and stable, and the success rate is high.

By using the scheme of the application, the Coriolis illusion experience training is carried out on the illusion simulator, which can help pilots to recognize, identify and correctly treat the illusions so as to effectively reduce the accident rate.

The embodiment of the application also discloses a storage medium which is a computer readable storage medium and is stored with a computer program, and the computer program can execute part or all of the steps of the method shown in fig. 2 when running. The storage medium may include Read-Only Memory (ROM), random access Memory (Random Access Memory, RAM), magnetic or optical disks, and the like. The storage medium may also include non-volatile memory (non-volatile) or non-transitory memory (non-transitory) or the like.

It is noted that the terms "comprises" and "comprising," and any variations thereof, in the description and claims of the present application and in the foregoing figures, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed or inherent to such process, method, article, or apparatus.

In this specification, each embodiment is described in a progressive manner, and identical and similar parts of each embodiment are all referred to each other, and each embodiment mainly describes differences from other embodiments. Moreover, the system embodiments described above are illustrative only, and the modules and units illustrated as separate components may or may not be physically separate, i.e., may reside on one network element, or may be distributed across multiple network elements. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of this embodiment. Those of ordinary skill in the art will understand and implement the present application without undue burden.

While the embodiments of the present application have been described in detail, the detailed description of the application is provided herein, and the description of the embodiments is provided merely to facilitate the understanding of the method and system of the present application, which is provided by way of example only, and not by way of limitation. All other embodiments, which can be made by those skilled in the art based on the embodiments of the present application without making any inventive effort, shall fall within the scope of the present application, and the present description should not be construed as limiting the present application. It is therefore contemplated that any modifications, equivalents, improvements or modifications falling within the spirit and principles of the application will fall within the scope of the application.

Claims (10)

1. A coriolis illusion simulation method, which is characterized by being used for a illusion simulator;

the method comprises the following steps:

receiving the setting operation of flight parameters by training personnel, and generating a target flight task;

sending first flight indication information to a trained person, so that the trained person finishes take-off operation according to information displayed by an instrument display system under the indication of the first flight indication information and keeps flying flatly after reaching a preset height;

sending second flight indication information to the trained personnel, so that the trained personnel enters a horizontal continuous turn in a flat flight stage according to information displayed by an instrument display system under the indication of the second flight indication information;

sending third flight indication information to the trained personnel so that the trained personnel generates Coriolis Li Cuojiao in the process of moving the head;

and sending fourth flight indication information to the trained personnel so as to enable the trained personnel to gradually eliminate the Coriolis illusion.

2. The coriolis illusion simulation of claim 1 wherein the target flight mission is a complex weather flight under diurnal preset weather parameters.

3. The coriolis illusion simulation of claim 2 characterized in that the pre-set complex weather conditions comprise any one of: flying in the cloud, flying on the cloud with cloud cover of more than 80 percent, and flying under the cloud with visibility of less than 5 km.

4. The coriolis illusion simulation of claim 1, wherein the target flight mission comprises: daytime complex meteorological flight tasks.

5. The coriolis illusion simulation of claim 1 wherein the predetermined height is greater than a cloud height.

6. The coriolis illusion simulation of claim 1 wherein the trained personnel entering a horizontal continuous turn in a flat flight phase based on information displayed by an instrumentation display system under the direction of the second flight indication information comprises:

the trained personnel rolls rapidly to the right or left to the maximum grade with an angular acceleration above the human perception threshold and maintains the altitude.

7. The coriolis illusion simulation of claim 6, wherein the flight simulator comprises: simulating a cabin, a six-degree-of-freedom motion platform and a 360-degree continuous rotation platform; the trained personnel entering a horizontal continuous turn in a flat flight stage according to the information displayed by the instrument display system under the indication of the second flight indication information further comprises:

and controlling the six-degree-of-freedom motion platform to drive the simulation cabin to roll to the right or left for inclination by a set angle, and simultaneously controlling the 360-degree continuous rotation platform to drive the simulation cabin to slowly accelerate to the right or left to a set angular speed at an angular acceleration below the human body feeling threshold value, and then continuously rotating at a constant speed.

8. The coriolis illusion simulation of claim 1 characterized in that said third flight indication information is used to instruct said trainee to quickly perform head movements.

9. The coriolis illusion simulation of claim 8, wherein the head motion comprises any one or more of: low head, head up, head swing right, head swing left.

10. The coriolis illusion simulation of claim 1 characterized in that said fourth indication is used to instruct said trainee to resume a head-up position, to trust instrument parameters, to continue to hold a turn flight.