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Pro108 antibody compositions and methods of use and use of Pro108 to assess cancer risk

This invention relates to a method for assessing risk of prostate cancer. Specifically, it relates to utilizing both Pro108 and Prostate Specific Antigen (PSA) in combination to determine the risk of prostate cancer. In addition, it is directed to a method for assessing risk of ovarian, colon, breast or stomach cancer utilizing Pro108 or specific antibodies to Pro108. The invention provides isolated anti-prostate, ovarian, colon, breast or stomach cancer antigen (Pro108) antibodies that bind to Pro108 on a mammalian cell in vivo. The invention also encompasses compositions comprising an anti-Pro108 antibody and a carrier. These compositions can be provided in an article of manufacture or a kit. Another aspect of the invention is an isolated nucleic acid encoding an anti-Pro108 antibody, as well as an expression vector comprising the isolated nucleic acid. Also provided are cells that produce the anti-Pro108 antibodies. The invention encompasses a method of producing the anti-Pro108 antibodies. Other aspects of the invention are a method of killing an Pro108-expressing cancer cell, comprising contacting Pro108 present in the ECM with an anti-Pro108 antibody and a method of alleviating or treating an Pro108-expressing cancer in a mammal, comprising administering a therapeutically effective amount of the anti-Pro108 antibody to the mammal.
Owner:DIAZYME LAB INC

Multi-level embedded integrated navigation system and navigation method

The invention discloses a multi-level embedded integrated navigation system and a navigation method, belonging to the technical field of integrated navigation. The method comprises the following steps: firstly establishing an aviation airborne inertial navigation system (INS) error state value equation and an inertia/satellite integrated measurement model, then defining a navigation error state value of an embedded inertia/satellite integrated system and establishing an inertia/star sensor integrated measurement model; on that basis, carrying out embedded inertia/satellite integrated system internal integrated navigation resolving and close-loop filtering correction, and finally carrying out external inertia/star sensor integrated navigation resolving and open-loop filtering correction to obtain multi-information fusion navigation results. According to the invention, the complete independent integrated structure of the embedded inertia/satellite integrated system can be kept, and simultaneously the multi-level fusion of inertia/satellite/astronomy asynchronous multi-sensor information and the step-by-step correction of the inertial navigation system are realized, the integrated navigation performance is effectively raised, and the invention is suitable for engineering application.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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