This invention relates to the integration of systems and, more particularly, to the integration of weapons on complex, highly integrated aircraft.
Integration of a weapon system with the other systems on an aircraft is a complex and lengthy task, as it affects all the major aircraft systems. Accordingly there is a requirement to improve weapon integration time and affordability.
One of the requirements of weapon integration is to enable the display of information to the aircraft pilot as to whether or not a weapon is capable of successfully engaging a particular target. For this purpose, weapons are usually grouped into two categories, weapons designed to engage targets on the ground (air to ground weapons) and weapons designed to engage targets in the air (air to air weapons). In the case of air to ground weapons, a Launch Acceptability Region (LAR) is calculated, being the region where the probability of successfully engaging or hitting a selected target is above some threshold value. The LAR is calculated in order to provide cockpit displays in the launch aircraft indicating the feasibility of successfully engaging the target, and is a function of the weapon performance characteristics, the relative positions and motions of the aircraft and the target, and often ambient conditions such as wind speed and direction.
For an air to air weapon, a Launch Success Zone (LSZ) is calculated, indicative of the probability of successfully engaging a selected air target is about some threshold value. Again the LSZ is used to provide a cockpit display indicating whether the weapon is capable of successfully engaging the target. However, calculation of a LSZ is more complicated than the calculation of a LAR, because the relative speeds and directions of travel of the launch aircraft and the target are much greater, and consequently the effects of ambient conditions are greater, and also the physical properties of the weapons in flight are more significant on the calculation.
The conventional approach has been to create a simple, abstract model of the weapon, which is modified according to the launch conditions (taking into account the aircraft and target conditions (e.g. range, direction and speed of travel, etc.) and the ambient conditions). The model is used on board the aircraft to generate the LAR or LSZ for display to the pilot. A disadvantage of the conventional approach is that each model, for each different weapon type, is different. Storing the data relating to several different implicit models consumes significant storage capacity, and each model has to be comprehensively integrated to ensure that there is no adverse effect on any of the aircraft systems. Further, if there are any changes or modifications made to a weapon (such as an improvement in performance) or if it is necessary to load the aircraft with a completely new weapon, a lengthy and expensive integration process has to be conducted because the weapon model is substantially different to anything previously integrated with the aircraft systems.
Accordingly, the present invention provides a system for generating in an aircraft in flight a display indicative of the feasibility of a weapon carried on the aircraft successfully engaging a determined target, the system comprising a first generator, which may be a ground station, for generating a database describing the weapon performance envelope, a second generator for creating coefficients characteristic of that performance envelope using a generic algorithm and means for uploading the coefficients to the aircraft, and a reconstructor on the aircraft containing the same generic algorithm and adapted to select the coefficients for the algorithm according to the aircraft and target conditions in order to generate the feasibility display, wherein the algorithm is generic to both air to ground and air to air weapons.
Such a system significantly improves weapon integration time and cost. A minimal number of generic weapon aiming algorithms are required in order to take account of all weapon types (air to air and air to surface, and powered or unpowered). The generic algorithms can be tailored to different weapons, depending on the weapon aiming methodology adopted, simply by changing the coefficients used in the algorithm. The coefficient can be implemented as loadable data so as to allow accurate and precise weapon behaviour to be implemented within the weapon system. Also, using one or only a few generic algorithms would allow different weapon systems to be cleared or certificated/qualified for use with the aircraft with reduced effort and more quickly than with the extensive testing which is required with conventional approaches. The use of generic algorithms for weapon aiming also enables increases or significant changes in weapon system capability to be integrated with the aircraft systems with significantly less effort then heretofore.
Preferably the algorithm is a standard polynomial of the form:
where:
αmn represent the m coefficients required to compute output n;
{x1 . . . xNi} represent the normalised inputs; and
The invention also provides, in a second aspect, a method for generating in an aircraft in flight a display indicative of the feasibility of a weapon carried on the aircraft successfully engaging a determined target comprising:
generating a database describing the weapon performance envelope;
creating coefficients characteristic of that performance envelope using a generic algorithm;
uploading to the aircraft the generated coefficients; and
reconstructing on the aircraft the performance envelope using the same generic algorithm and, according to the aircraft and target conditions and the performance envelope, generating the feasibility display, wherein the algorithm is generic to both air to ground and air to air weapons.
The aircraft and target conditions may include one or more of their relative positions, distances, directions of movement, speeds and ambient atmospheric conditions.
The coefficients specific to a weapon are preferably uploaded to the aircraft when the weapon is loaded as a weapon store. All that is required when loading a new weapon store to integrate the weapon and aircraft aiming system is at the same time to load the coefficients associated with that weapon into the aircraft system; ideally the coefficient could be stored on a hardware device with the weapon, and the devise connected to the aircraft to upload the coefficient data as the weapon is loaded.
The database may be generated by defining the range of conditions for which the weapon may be required to be fired, the range of aircraft conditions for which it is feasible for the aircraft to fire the weapon and the range of weapon conditions for which it is feasible to fire the weapon;
generating data indicative of the weapon performance for each weapon firing possibility from within the defined ranges, and creating a database defining the weapon's overall performance envelope.
In this way the database can be generated on a ground-based system, so that the aircraft system needs the capacity only to store the algorithm and process the coefficients with the aircraft and target conditions in order to generate the feasibility display, thus reducing the amount of data storage/processing capacity required on the aircraft.
The method may also comprise inputting into the reconstructor coefficients characteristic of the performance envelope of a weapon carried by another aircraft, reconstructing that performance envelope using the generic algorithm and, according to the conditions of both aircraft and the performance envelope, generating a display indicating the feasibility of the aircraft being successfully engaged by the weapon on the other aircraft.
In this way, the same aircraft system can also display whether or not, or to what extent, the aircraft is at risk of being successfully engaged by a weapon carried by a hostile aircraft, which may be a hostile aircraft which the host aircraft is deciding whether or not to engage. The generic algorithm enables the calculation of opposing LSZs and allows better assessment of air to air engagements. This in turn could lead to confident predictions of advantage and likely outcome of engagements.
The invention also encompasses an aircraft comprising the above described systems and methods.
An embodiment of the invention will now be described by way of example and with reference to the accompanying drawings, in which:
a and 1b illustrate the Launch Acceptability Region (LAR) for an air to surface weapon;
a shows the LAR in the plane of flight of a launch aircraft 1 flying along a flight path 3 in respect of a target 5 for an air to surface weapon (not shown) loaded on the aircraft. The LAR is calculated to provide cockpit displays in the launch aircraft 1 concerning the feasibility and firing opportunities for the situation.
The LSZ shown in
As is known in the art, there are two LSZs, one for the launch aircraft to engage the target 7 and the other for the target to engage the launch aircraft.
It is often a requirement to calculate the LAR or LSZ for an engagement to display to the crew of the launch aircraft information regarding the feasibility, or likelihood of success, of the engagement, and to aid fire control and steering decisions. The traditional approach has been to create a simple, abstract model of the weapon that has parameters defined by the launch conditions; this model is then used on board the launch aircraft to generate the LAR or LSZ and the appropriate display.
In the present invention a coefficient generator 21 receives the true weapon performance envelope represented by the truth database and calculates and generates coefficients according to a generic LAR/LSZ algorithm 23—the coefficients “fit” the generic algorithm to the weapon performance envelope shape.
The coefficient generator 21 may generate coefficients by building training and verification footprints (representing the target engagement envelope) from data extracted from the truth database, by fitting a geometric shape to the training footprint and by defining the coefficients for the generic algorithm. The coefficient generator then verifies the coefficients against the verification sets by creating footprints based on the coefficients at the verification set conditions and by confirming that these verification footprints meet the criteria for successful engagement.
In an alternative method of coefficient generation, illustrated in
The Genetic Algorithm is applied to the candidate polynomials and scores. The best polynomials are retained and the worst rejected. New candidates that have similar features to the retained candidates are created to replace the rejected ones. The coefficients giving the least squares fit and the scores are then calculated for this new generation of candidates.
The Genetic Algorithm is repeated until improvement in the scores of the best candidates ceases. The result is the first layer, Layer 1, of a Self-Organising Polynomial Neural Network (SOPNN) where each node describes a polynomial function that relates the weapon or aircraft firing condition parameters to a characteristic of the required LAR/LSZ.
The whole process is then repeated with the outputs of the first layer providing the inputs to create a second layer, Layer 2, of the SOPNN. The new layer has the effect of creating higher-order candidate polynomials and coefficients for consideration. The selection of polynomials in the new layer is again governed and optimised by the Genetic Algorithm.
Layers are added to the SOPNN in this way until improvement in the scores of the best candidates ceases—a completed network comprising two layers is represented in
The best single candidate polynomial and coefficient set is identified and stored. This process is repeated until all the required characteristics of the LAR/LSZ have corresponding polynomial models.
The generic LAR/LSZ algorithm is predetermined, and in the present invention is a polynomial equation of the form:
Where:
αmn represent the m coefficients required to compute output n;
{x1 . . . xNi} represent the normalised inputs; and
Referring again to
Number | Date | Country | Kind |
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09251978.4 | Aug 2009 | EP | regional |
0914109.4 | Aug 2009 | GB | national |
0921089.9 | Dec 2009 | GB | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/GB10/51323 | 8/10/2010 | WO | 00 | 5/29/2012 |