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88 results about "Product term" patented technology

In Boolean logic, a product term is a conjunction of literals, where each literal is either a variable or its negation.

Beamforming and interference cancellation system using general purpose filter architecture

A beamforming system including a multiplier stage for providing a plurality of steered signal terms, each term being a product of an input signal term and a steering signal term. A filter multiplies the steered signal terms by a plurality of respective filter weights to provide a plurality of weighted products. The weighted products are summed to provide an output beam directionally responsive to the steering signal. A microprocessor provides the steering signal terms and the filter weights in response to the input signal and/or user input. In the preferred embodiment, the filter is a reconfigurable, general purpose matched filter configured to multiply a plurality of delayed representations of a respective one of the steered signal terms by a plurality of the weights to provide a plurality of intermediate weighted product terms. The filter further includes a summing circuit for accumulating the intermediate weighted product terms to provide a respective one of the plurality of weighted products. The inventive beamforming system cancels unwanted interference, while forming a beam to allow a desired signal to be received with a maximum signal-to-interference-plus-noise ratio (SINR). Through a data-capture RAM, the system allows interference samples to be collected and passed to a microprocessor to calculate the optimum filter weights. The received beam may be steered to any desired direction to form an optimal space-time adaptive matched filter.
Owner:RAYTHEON CO

Rotational inertia frequency domain detection method based on floating torsion pendulum table

The invention provides a rotational inertia frequency domain detection method based on a floating torsion pendulum table, belonging to the technical field of rotational inertia detection. According to the method, a problem that an existing time domain measurement method of torsion method rotational inertia is influenced by a cycle measurement precision and finally the measurement precision of the rotational inertia is influenced is solved. The technical points of the method are that in the condition of a damping linear model, a pendulum motion differential equation can be written according to the law of rotation, the equation is solved to obtain the function of pendulum motion angle about time, an expression is subjected to approximate processing, a product term is subjected to power series expansion and a higher-order term is neglected, then the expression is subjected to continuous Fourier transform to obtain an analysis formula, finally the magnitude of the undamped natural vibration frequency of a detected product can be calculated according to the peak frequency and damping ratio, and the magnitude of the product rotational inertia is obtained. The method is mainly applied to the rotational inertia measurement of an air vehicle such as a missile, an interceptor and an unmanned aerial vehicle and can be applied to the rotational inertia measurement of other large equipment.
Owner:严格集团股份有限公司

ESOP minimization method for logic function

The present invention discloses an ESOP minimization method for a logic function. By converting the optimal coverage searching problem of a 3n global space in the ESOP minimization process of an n variable logic function into the simplest connection problem in a plurality of cube blocks, a search space is reduced, thereby breaking away from a constraint of a variable scale; moreover, a cube set is directly operated without being converted into a minterm set, so that limitation to a product term number is avoided; and in order to achieve accurate minimization of rapid ESOP, a minimized conversion algorithm of a cube EXOR conversion diagram is adopted to improve operation efficiency so as to effectively reduce calculation complexity and a memory occupied quantity, and the characteristics that calculation time is insensitive to the number of input variables and is only related to the number of product terms included by the logic function and intersection can effectively achieve an effect that random n variables totally regulate the ESOP minimization of the logic function. The ESOP minimization method has the advantages of no limitation to the number of the product items and the number of the variables in the logic function and capacity of carrying out minimization processing on an ESOP of a random logic function.
Owner:ZHEJIANG WANLI UNIV

Aircraft aerodynamic characteristic on-line identification method based on backtracking self-adaptive algorithm

The invention provides an aircraft aerodynamic characteristic on-line identification method based on a backtracking self-adaptive algorithm. The aircraft aerodynamic characteristic on-line identification method comprises steps: (1) equivalently transforming the product term of the inverse of a rotational inertia matrix and a moment vector in an aircraft angular velocity kinetic equation into a Phi<T>(k)Theta* form, carrying out discretization processing on the transformed product term, and obtaining an aircraft angular velocity difference equation; wherein Phi<T>(k) represents a signal vector,Theta* represents a parameter truth vector, and the parameter truth vector is a column vector including an aerodynamic characteristic parameter to be identified; (2) establishing a mathematical modelof an angular velocity estimation virtual system, and making an angular velocity estimation error and a parameter estimation error be Phi<T>(k)[Theta(k)-Theta*], wherein Theta(k) represents an estimated value of the parameter truth vector; (3) establishing a backtracking performance formula of the angular velocity estimation error, combining a backtracking updating rule to obtain Phi (k) in realtime, resolving the Theta(k) by means of the backtracking self-adaptive algorithm, making the angular velocity estimation error omega-wave(k) approach zero, and resolving the aerodynamic characteristic parameter to be identified according to the value of the Theta(k). The aircraft aerodynamic characteristic on-line identification method has a lower calculated amount and a lower demand on the computer, and has operability.
Owner:BEIJING LINJIN SPACE AIRCRAFT SYST ENG INST +1
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