초록 ▼

In an iterative method of determining aircraft flight data parameters using first and second multi-function probes, an assumed value of a first aircraft parameter is defined to be equal to an initial value. Using the assumed value of the first aircraft parameter together with the respective local an

In an iterative method of determining aircraft flight data parameters using first and second multi-function probes, an assumed value of a first aircraft parameter is defined to be equal to an initial value. Using the assumed value of the first aircraft parameter together with the respective local angles of attack determined at first and second multi-function probes, first and second estimates of a second aircraft parameter are calculated and compared. If the first and second estimates of the second aircraft parameter are within tolerance of each other, then the first aircraft parameter is approximately equal to the assumed value, and the second aircraft parameter is determined from the first and second estimates. If the first and second estimates of the second aircraft parameter are not within tolerance of each other, then an iterative process is continued to correctly determine the first and second parameters.

대표청구항 ▼

In an iterative method of determining aircraft flight data parameters using first and second multi-function probes, an assumed value of a first aircraft parameter is defined to be equal to an initial value. Using the assumed value of the first aircraft parameter together with the respective local an

In an iterative method of determining aircraft flight data parameters using first and second multi-function probes, an assumed value of a first aircraft parameter is defined to be equal to an initial value. Using the assumed value of the first aircraft parameter together with the respective local angles of attack determined at first and second multi-function probes, first and second estimates of a second aircraft parameter are calculated and compared. If the first and second estimates of the second aircraft parameter are within tolerance of each other, then the first aircraft parameter is approximately equal to the assumed value, and the second aircraft parameter is determined from the first and second estimates. If the first and second estimates of the second aircraft parameter are not within tolerance of each other, then an iterative process is continued to correctly determine the first and second parameters. achable voltage regulator module comprises a circuit that instructs the voltage regulator module to regulate a first voltage level to a second voltage level. 15. The apparatus of claim 10, wherein the circuit is programmable by the microprocessor. 16. The apparatus of claim 10, wherein the detachable voltage regulator module and socket connector may be mounted in either a horizontal or vertical plane. 17. The apparatus of claim 10, where in the apparatus is positioned in a plane paralleled to air flow of the microprocessor. 18. An apparatus for regulating voltage in an electronic device, comprising: a detachable voltage regulator module having a receptacle assembly mounted on the detachable voltage regulator module; and a socket connector, residing on a same board and coupled to the electronic device, having an opening that receives the receptacle assembly and interfaces the detachable voltage regulator module with the electronic device. 19. The apparatus of claim 18, wherein the receptacle assembly comprises a plurality of receptacles that receives a plurality of pins from the socket connector. 20. The apparatus of claim 18, wherein the socket connector comprises a plurality of pins that allow the socket connector to interface with the receptacle assembly. 21. A computer system comprising: a bus; a microprocessor coupled to the bus; a memory coupled to the bus; and a voltage regulating device, residing on a same board and coupled to the microprocessor, comprising a detachable voltage regulator module having a receptacle assembly mounted on the detachable voltage regulator module, and a socket connector having an opening that receives the receptacle assembly and interfaces the detachable voltage regulator module with the microprocessor. 22. The computer system of claim 21, wherein the receptacle assembly comprises a plurality of receptacles that receives a plurality of pins from the socket connector. 23. The computer system of claim 21, wherein the socket connector comprises a plurality of pins that allow the socket connector to interface with the receptacle assembly. cording to claim 1, wherein the articles (1, 2) are placed in a predetermined sequence onto the supports (3). 10. The method according to claim 9, wherein the articles are placed according to a placement algorithm onto the supports (3). 11. The method according to claim 1, wherein the control unit (7) controls several of the gripping devices (9, 19, 29, 39). 12. The method according to claim 11, wherein each one of the articles (1, 2) has correlated therewith a predetermined one of the gripping devices (9, 19, 29, 39). 13. The method according to claim 1, further comprising the steps of: performing simulations in the control unit (7) before the step of carrying out a placement step, wherein the simulations are virtual placement steps of placing the articles (1, 2) onto the supports (3) carried out by the gripping devices (9, 19, 29, 39) connected to the control unit (7); selecting by the control unit (7) one of the simulations, based on the predetermined criteria, as an optimal placement process; and, in the step of controlling, moving the gripping device (9, 19, 29, 39) according to the optimal placement process. 14. The method according to claim 13, wherein the simulations are carried out by neuronal operations, fuzzy logic operations, or neuronal and fuzzy logic operations. 15. The method according to claim 13, wherein the predetermined criteria of the control unit (7) comprise data derived from the simulations and data derived from prior placement processes. 16. The method according to claim 13, wherein the simulations process at least one of product-specific parameters, configuration-related parameters of the gripping device, position-dependent parameters of the gripping device, and movement-dependent parameters of the gripping device. 17. The method according to claim 13, wherein the simulations are carried out according to a boolean operation. 18. The method according to claim 17, wherein the simulations are carried out according to an algorithm.