Aircraft flight emulation test system

Claim 2

An aircraft test system for evaluating the performance of an aircraft on the ground, the aircraft having a number of different aircraft components to which stimuli is applied and that, in reaction to the stimuli, generate measurable responses, including: a plurality of processor-controlled test instruments for generating different stimuli to which the aircraft components are exposed in flight including at least one instrument for generating at least one radio navigation signal received by an aircraft component, at least one instrument for generating an airflow monitored by an aircraft component, and at least one instrument for generating an electrical signal normally generated by a first aircraft component that is received by a second aircraft component; a plurality of test instruments for measuring the response of the aircraft components to the stimuli to which they are exposed and for producing output signals representative of said measurements; and, processor means connected to said stimuli generating test instruments for controlling said test instruments and to said aircraft measuring test instruments for receiving said output signals representative of the measured responses of the aircraft components wherein, said processor means maintains an aircraft state vector containing a plurality of aircraft state variables, each said aircraft state variable describing a particular in-flight attribute of the aircraft, said processor means periodically produces updated said aircraft state variables based on the aircraft state vector at the start of the update process and the measured responses of the aircraft components, and said processor means adjusts the stimuli applied to the aircraft components based on said updated aircraft state variables so that the stimuli applied to the aircraft components emulates the stimuli applied to aircraft components when the aircraft is in flight.

Claim 3

The aircraft test system of claim 1, wherein at least one of said stimuli generating test instruments generates airflows simulating pitot and static air flows monitored by an aircraft component.

Claim 4

The aircraft test system of claim 2, wherein at least one said stimuli generating test instrument generates signals normally generated by an on-aircraft inertial navigation reference unit.

Claim 5

The aircraft test system of claim 3, further including an operator interface means connected to said processor means for allowing an operator to control the generation of stimuli through said processor means.

Claim 6

The air data system of claim 3, wherein at least one said stimuli generating test instrument receives radio altimeter interrogation signals emitted by the aircraft and transmitted return radio altimetry interrogation signals to the aircraft based on a time delay that emulates the in-flight emission and reception of signals by the aircraft.

Claim 7

The aircraft test system of claim 5, wherein at least one said stimuli generating instrument generates instrument landing, glide slope and localizer signals emulating the glide slope and localizer signals normally received by the aircraft.

Claim 8

The aircraft test system of claim 6, further including at least one said stimuli generating instrument for generating engine performance signals emulating engine performance signals normally transmitted by an aircraft engine to another component of the aircraft.

Claim 9

The aircraft test system of claim 7, wherein: at least one of said measuring instruments is adapted for connection to the aircraft for receiving command signals sent between aircraft components; and said processor means is further adapted to produce said updated aircraft state variables in response to the commands transferred between the aircraft components that are monitored by said measuring instrument that receives said commands.

Claim 10

The aircraft test system of claim 7, further including at least one said measuring test instrument for recording signals from an aircraft component that are normally read for storage by an on-aircraft flight data acquisition unit; a flight data reader connected to the aircraft flight data acquisition unit for reading the data stored by the flight data acquisition unit; and, said processor means is connected to said flight data reader for reading the flight data recorded from said flight data reader and comparing said data with said measuring instrument output signals.

Claim 11

The aircraft test system of claim 1, wherein said aircraft state vector includes a plurality of instrument input parameters, wherein each said input parameter describes an attribute of a specific stimulus that is generated by said stimuli generating instruments, and said processor means adjusts the application of stimuli to the aircraft components by initially updating at least one of said aircraft state variables updating at least one instrument input parameter based on said updated aircraft state variable, and adjusting at least one of said stimuli generating instruments based on said updated instrument input parameter.

Claim 12

The aircraft test system of claim 10, wherein: at least one said stimuli generating instrument has a lag between the time at which said instrument is directed to adjust said stimuli applied to the aircraft and time at which said adjusted stimuli is applied to the aircraft; and said processor means produces control signals for controlling stimuli generated by said lagging stimuli generating instrument based on a predictor equation from which control signals are produced to overdrive said stimuli generating instrument so that said stimuli generating instrument will produce stimuli approximately equal to said real time stimuli.

Claim 13

The air data test system of claim 11, wherein said stimuli generating instrument for producing said airflow is said lagging instrument and said processor means controls production of said airflow based on a set of air data lag predictor equations.

Claim 14

The aircraft test system of claim 10, wherein: said aircraft state vector includes a plurality of aircraft input variables, each said aircraft input variable describing aircraft information measured by said system measuring instruments; and said processor means updates said aircraft state vector in a series of flight emulation frames wherein, in each said flight emulation frame said processor means produces updated aircraft state variables based on said aircraft input variables and said aircraft state variables at the beginning of said frame and produces updated instrument input parameters based on said updated aircraft state variables.

Claim 15

The aircraft test system of claim 13, wherein during said flight emulation frames said processor means adjusts said stimuli generating instruments based on said updated instrument input parameters and said processor means updates at least one said stimuli generating instrument at a rate less than once every said flight emulation frame.

Claim 16

The aircraft test system of claim 14, wherein during said flight emulation frames said processor means updates said aircraft input variables based on measurements made by said test instruments and said processor means updated at least one said aircraft input variable at a rate less than once every flight emulation frame.

Claim 17

The aircraft test system of claim 15, wherein said processor means is provided with an interface unit for allowing manual entry of start point data, and said processor means produces an initial aircraft state vector based on said start point data and wherein said processor means generates a subsequent said aircraft state vectors based on said initial aircraft state vector.

Claim 18

The aircraft test system of claim 13, wherein during said flight emulation frames said processor means updates said aircraft input variables based on said measurements made by said test instruments and said processor means updates at least one said aircraft input variable at a rate less than once every said flight emulation frame.

Claim 19

The aircraft test system of claim 1, wherein said processor means is provided with an interface unit for allowing manual entry of start point data, and said processor means produces an initial aircraft state vector based on said start point data, and said processor means generates a subsequent said aircraft state vector based on said initial aircraft state vector.

Claim 20

An aircraft test system for emulating the in-flight performance of an aircraft on the ground, the aircraft including a plurality of aircraft components to which stimuli is applied and that in reaction to the stimuli, generate measurable responses, said system including: a plurality of processor-controlled test instruments generating the stimuli to which the aircraft components are exposed to in flight, including a test instrument for generating a radio signal received by an aircraft navigation receiver, a test instrument for generating an airflow monitored by an aircraft component, and an instrument for generating an electrical signal produced by a first aircraft component that is received by a second aircraft component; a plurality of monitoring instruments for measuring the response of aircraft components to the stimuli to which they are exposed and for producing output signals representative of said measurements, wherein at least one of said measuring test instruments is connected to an aircraft component different than the aircraft components to which stimuli is applied; and a processor unit connected to said stimuli generating test instruments for controlling said test instruments and said aircraft measuring test instruments for receiving said output signals therefrom, wherein said processing unit maintains a plurality of aircraft state variables, each said aircraft state variable describing a particular in-flight attribute of the aircraft, a plurality of aircraft input variables, each said aircraft input variable describing aircraft information measured by said measuring instruments, and a plurality of instrument input parameters, each said instrument parameter describing an attribute of a specific stimuli generated by one of said stimuli-generating instruments, and said processor means continually changes the stimuli applied to the aircraft components in a series of flight emulation frames, wherein in each flight emulation frame said aircraft state variables are updated based on said aircraft state variables at the beginning of said frame and said aircraft input variables and said instrument input parameters are updated based on said updated aircraft state variables and wherein during selected flight emulation frames, said processing unit said updates said aircraft input variables based on the measurements made by said monitoring instruments and adjusts said stimuli-generating instruments based on said updated instrument input parameters.

Claim 21

An aircraft test system for emulating the in-flight performance of an aircraft on the ground, the aircraft including a plurality of aircraft components to which stimuli is applied and that in reaction to the stimuli, generate measurable responses, said system including: a plurality of processor-controlled test instruments generating the stimuli to which the aircraft components are exposed to in flight, including a test instrument for generating a radio signal received by an aircraft navigation receiver, a test instrument for generating an airflow monitored by an aircraft component, and an instrument for generating an electrical signal produced by a first aircraft component that is received by a second aircraft component; a plurality of monitoring instruments for measuring the response of aircraft components to the stimuli to which they are exposed and for producing output signals representative of said measurements, wherein at least one of said measuring test instruments is connected to an aircraft component different than the aircraft components to which stimuli is applied; and a processor unit connected to said stimuli generating test instruments for controlling said test instruments and said aircraft measuring test instruments for receiving said output signals therefrom, wherein said processing unit maintains a plurality of aircraft state variables, each said aircraft state variable describing a particular in-flight attribute of the aircraft, a plurality of aircraft input variables, each said aircraft input variable describing aircraft information measured by said measuring instruments, and a plurality of instrument input parameters, each said instrument parameter describing an attribute of a specific stimuli generated by one of said stimuli-generating instruments, and said processor means continually changes the stimuli applied to the aircraft components in a series of flight emulation frames, wherein in each flight emulation frame said aircraft state variables are updated based on said aircraft state variables at the beginning of said frame and said aircraft input variables and said instrument input parameters are updated based on said updated aircraft state variables and wherein during selected flight emulation frames, said processing unit said updates said aircraft input variables based on the measurements made by said monitoring instruments and adjusts said stimuli-generating instruments based on said updated instrument input parameters.

Claim 22

The aircraft test system of claim 19, wherein said aircraft input variables are updated at a rate less than once every flight emulation frame.

Claim 23

The aircraft test system of claim 19, wherein a first one of said stimuli-generating test instruments is updated at a first rate, a second one of said stimuli generating instruments is updated and wherein said rates at which said first and second stimuli generating test instruments are updated is different and said first and second stimuli generating instruments are updated at rates less than once every flight emulation frame.

Claim 24

The aircraft test system of claim 19, wherein said aircraft input variables are updated at a rate less than once every flight emulation frame.