Ex Parte DiggelenDownload PDFPatent Trial and Appeal BoardMar 12, 201813026050 (P.T.A.B. Mar. 12, 2018) Copy Citation United States Patent and Trademark Office UNITED STATES DEPARTMENT OF COMMERCE United States Patent and Trademark Office Address: COMMISSIONER FOR PATENTS P.O.Box 1450 Alexandria, Virginia 22313-1450 www.uspto.gov APPLICATION NO. FILING DATE FIRST NAMED INVENTOR ATTORNEY DOCKET NO. CONFIRMATION NO. 3875.4560001 4017 EXAMINER ISSING, GREGORY C ART UNIT PAPER NUMBER 3646 MAIL DATE DELIVERY MODE 13/026,050 02/11/2011 Frank van Diggelen 26111 7590 03/13/2018 STERNE, KESSLER, GOLDSTEIN & FOX P.L.L.C. 1100 NEW YORK AVENUE, N.W. WASHINGTON, DC 20005 03/13/2018 PAPER Please find below and/or attached an Office communication concerning this application or proceeding. The time period for reply, if any, is set in the attached communication. PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte FRANK VAN DIGGELEN Appeal 2017-000642 Application 13/026,050 Technology Center 3600 Before BRETT C. MARTIN, LYNNE H. BROWNE, and THOMAS F. SMEGAL, Administrative Patent Judges. SMEGAL, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE Frank Van Diggelen (Appellant)1 seeks our review under 35 U.S.C. § 134 of the Examiner’s rejections2 under 35 U.S.C. § 112, first paragraph, of claims 1—9, 11—19, 21, and 22 as failing to comply with the written description requirement; under 35 U.S.C. § 102(b) of claims 1—3, 9, 11—13, 19, 21, and 22 as anticipated by Raman (US 2009/0115656 Al, pub. May 7, 1 According to Appellant, the real party in interest is Broadcom Corporation, Appeal Br. 4. 2 Appeal is taken from the adverse decision of the Examiner as set forth in the Non-Final Office Action, dated December 24, 2014 (“Non-Final Act.”), as further modified by the Advisory Action, dated September 16, 2015 and the Final Office Action, dated June 5, 2015 (“Final Act.”). Appeal 2017-000642 Application 13/026,050 2009); and under 35 U.S.C. § 103(a) of claims 4—8 and 14—18 as unpatentable over Raman and Liccardo (US 8,065,074 Bl, iss. Nov. 22, 2011).3 We have jurisdiction under 35 U.S.C. § 6(b). We AFFIRM. CLAIMED SUBJECT MATTER Claims 1,11, and 21 are independent. Claim 1, reproduced below, illustrates the claimed subject matter, with disputed limitations emphasized. 1. A method comprising: collecting global navigation satellite system (GNSS) measurement data based on a GNSS signal received by a GNSS radio; collecting non-GNSS sensor data based on a non-GNSS signal received by a non-GNSS sensor; formatting the collected non-GNSS sensor data into a data format that is compliant with a format of the collected GNSS measurement data; computing hybrid navigation information based on the collected GNSS measurement data and the formatted non-GNSS sensor data; estimating expected non-GNSS sensor data based on the hybrid navigation information; and calibrating the non-GNSS sensor using the hybrid navigation information in response to determining the expected non-GNSS sensor data does not match the collected non-GNSS sensor data. 3 Claims 10 and 20 were canceled. See Appeal Br. 25, 27. 2 Appeal 2017-000642 Application 13/026,050 ANALYSIS First Ground of Rejection: Lack of Written Description of Claims 1—9, 11-19, 21, and 22 We are persuaded by Appellant’s arguments that the Examiner erred in rejecting claims 1—9, 11—19, 21, and 22 under 35 U.S.C. § 112, first paragraph, as failing to comply with the written description requirement. The purpose of the written description requirement in 35 U.S.C. § 112, first paragraph, is to ‘“clearly allow persons of ordinary skill in the art to recognize that [the inventor] invented what is claimed.’” AriadPharms., Inc. v. Eli Lilly and Co., 598 F.3d 1336, 1351 (Fed. Cir. 2010) (en banc) (quoting Vas-Cath, Inc. v. Mahurkar, 935 F.2d 1555, 1563 (Fed. Cir. 1991)). “[T]he test for sufficiency is whether the disclosure of the application relied upon reasonably conveys to those skilled in the art that the inventor had possession of the claimed subject matter as of the filing date.” Id. The Examiner contends that “[regarding the independent claims 1, 11 [,] and 21, the step of ‘'estimating expected non-GNSS sensor data based on the hybrid navigation information'' is insufficiently disclosed in the specification as originally filed,” thereby failing “to sufficiently describe how the expected or derived non-GNSS sensor data is estimated based on the hybrid navigation information.” Non-Final Act. 2. Although acknowledging that “the specification describes such [an] intended result at . . . [paragraph 41] by the language fijn step 504, the conformance driver 322 may derive or estimate navigation information expected in the collected non-GNSS sensor data based on the navigation information output from the GNSS application or function 326, ’” the Examiner finds that “the [Specification] fails to adequately teach any manner in which the 3 Appeal 2017-000642 Application 13/026,050 expected/derived data is estimated,” and observes that “[t]he remaining portion of that paragraph simply refers to the use of the derived navigation information.” Id. at 2—3. Based upon the foregoing, the Examiner concludes that “[t]he specification merely identifies steps that appear to correspond to the claim language but does not describe the claimed invention in sufficient detail that one skilled in the art can reasonably conclude that the inventor had possession of the claimed invention.” Id. at 8. In taking issue with the Examiner’s findings and conclusions, Appellant contends “[t]he claims satisfy § 112, | l’s written description requirement because the Specification demonstrates that the Inventor was in possession of the claimed invention-including the disputed ‘estimating’ and ‘calibrating’features.” Appeal Br. 11. More specifically, Appellant explains that “[a]s shown in the claim charts in Section III(B) of this Appeal Brief, the Specification provides ample support for the claimed features, including the disputed ‘estimating’ and ‘calibrating’ features.” Id. at 13. Appellant also reasons that “the Examiner's concern, leading to the outstanding § 112 rejections, is that the disputed features are (allegedly) ‘insufficiently described’ in the Specification,” which would “at best challenge [] enablement, not written description.” Id. We agree with Appellant that challenging the enablement requirement “requires an analysis of the Wands factors to determine whether a person of ordinary skill in the art can make and use the invention without undue experimentation.” Id. (citing In re Wands, 858 F.2d 731 (Fed. Cir. 1988)). However, as Appellant points out, “the Examiner has not analyzed the Wands factors to show that 4 Appeal 2017-000642 Application 13/026,050 undue experimentation is required to practice the ‘estimating’ and ‘calibrating’ features.” Id. Based on the foregoing, we do not sustain the Examiner’s rejection of claims 1—9, 11—19, 21, and 22 under 35 U.S.C. § 112, first paragraph, as failing to comply with the written description requirement. Second Ground of Rejection: Anticipation of Claims 1—3, 9, 11—13, 19, 21, and 22 by Raman Appellant initially argues claims 1—3, 9, 11—13, 19, 21, and 22 together in contesting the rejection of these claims as anticipated by Raman. See Appeal Br. 14—18; Reply Br. 3—4, 5—8. We select claim 1 as the representative claim for this group, and the remaining claims stand or fall with claim 1. See 37 C.F.R. § 41.37(c)(l)(iv). Appellant also presents additional arguments for dependent claims 3,9, 13, and 22 (Appeal Br. 18— 19), which we address infra. The Examiner finds that Raman discloses a method for determining a position using a device illustrated in Figure 3 that includes a GNSS receiver (330) for collecting the GNSS measurement data, inertial sensors (310) for collecting non- GNSS sensor data, navigator (315) for formatting the collected non-GNSS sensor data into a data format (317) compliant with a format of the GNSS data (337), a mixer (320) for computing hybrid navigation information and a navigation filter (340), such as a Kalman filter, that can generate and transmit feedback information (310) relating to accelerometer and gyro drift correction. Non-Final Act. 9-10 (citing Raman || 28, 35). The Examiner also determines that “navigation filter (340) estimates position, velocity, attitude and accelerometer and gyro errors [0025],” while 5 Appeal 2017-000642 Application 13/026,050 “inertial sensors (310) can use the information related to accelerometer and gyroscope drift correction for calibration of the inertial sensor, leading to better inertial measurements.” Id. at 10. Furthermore, the Examiner reasons that Raman’s disclosure of the navigation filter transmitting feedback information to the non-GNSS sensors for the purpose of calibrating such as well as the fact that the navigation filter estimates, due to the predictive processing afforded by a Kalman filter, position, velocity, [and] sensor errors is deemed to disclose the claimed steps of “estimating expected non-GNSS sensor data” as well as “calibrating the non-GNSS sensor using the hybrid navigation information.” Id. From the foregoing, the Examiner concludes that “the calibration, which is a process for correcting/compensating erroneous information, occurs only in response to an error between the sensor data and the estimated data and thus anticipates the claims.” Id. In contesting the rejection, Appellant first argues that the § 102(b) rejection “improperly combine[s] elements from different embodiments of Raman,” including “elements from the apparatus of FIG. 3 of Raman and steps from the method of FIG. 8 of Raman [that are used] to reject the independent claims.” Appeal Br. 14. However, we agree with the Examiner that “[t]he rejection sets forth the steps of the method on the basis of identifying examples associated with Fig. 8,” that include “structural components that are capable of providing the information associated with the claimed method are a processor, a GNSS radio, and a non-GNSS sensor.” Ans. 13. In particular, the Examiner reasons, “[t]he embodiments of FIGs. 5 and 7 differ from the embodiment of FIG. 3 only in the inclusion of adding differential correction, locally (FIG. 6 Appeal 2017-000642 Application 13/026,050 5), or globally (FIG. 7), and merely correspond to using correction values via the steps 815/820,” while “the operation of the remaining elements [of Fig. 8] do not change.” Based on the foregoing, we agree with the Examiner that “Appellant’s argument is not convincing.” Id. at 13—14. Appellant next contends that “Raman fails to disclose ‘formatting the collected non-GNSS sensor data into a data format that is compliant with a format of the collected GNSS measurement data,’” as recited by the independent claims, because “neither step 810 nor step 830 is directed to formatting data from Raman’s inertial sensor(s),” as “they are directed to deriving new data.” Appeal Br. 15; Reply Br. 5—6. Appellant reasons “[s]ince deriving new data (i.e., the estimates of steps 810 and 830) is not the same as formatting data (as recited in the independent claims),” that “Raman fails to disclose the ‘formatting’ feature of the independent claims.” Appeal Br. 15. In response, the Examiner explains that “the processing of the measurement data [by Raman], either GNSS or inertial, into a position and velocity is deemed to equate to the formatting of the inertial sensor data to the same form as the GNSS data.” Ans. 14. The Examiner reasons that while arguing “that this is not the same as formatting the data, Appellant fails to show how or why the Office’s statement of such differs from the Appellant’s interpretation,” pointing out that “[according to the Appellant’s own specification, ‘ [t] he GNSS enabled device 112 may convert the WiFi measurements to position data, velocity data and/or time data in accordance with the GNSS measurement data format/'1' Id. We agree with the Examiner that “the teachings in Raman . . . which convert measurements from data collected from an inertial sensor (step 805) into position and 7 Appeal 2017-000642 Application 13/026,050 velocity estimates (step 810) are equivalent to the Appellant’s own teachings.” Id. Appellant continues by contending the “§ 102 rejections are deficient on their face because they do not point to a specific teaching in Raman that discloses ‘estimating expected non-GNSS sensor data based on the hybrid navigation information,’” asserting that “Raman’s mere disclosure of a Kalman filter. . . does not explicitly disclose that the Kalman filter performs the claimed ‘estimating,’” and concludes that “Raman's mere disclosure of a Kalman filter does not teach this specific feature.” Appeal Br. 16; Reply Br. 6-8. While also asserting that “the Final Office Action [improperly] introduced a second ‘reference’ in the form of two illegible, cut-and-paste slides downloaded from the Internet that allegedly teaches the ‘conventional operations’ of a Kalman filter,” Appellant argues “nowhere do these slides teach that Kalman filters necessarily estimate ‘expected non-GNSS sensor data based on the hybrid navigation information’” (id. at 16—17). Appellant also contends “the Examiner has not established that [the] slides are prior art.” Id. at 17. In response, the Examiner first explains “the rejection sets forth the use of mixer 320 and a Kalman filter 340.” Ans. 15 (citing Raman || 27, 28). The Examiner reasons that since the instant specification is silent as to the manner in which the expected non-GNSS sensor data is estimated based on the hybrid navigation information, such must be read in its broadest reasonable interpretation and as best understood by the . . . Examiner, the Kalman filter of Raman meets the scope of the claimed subject matter since, as a predictive navigation filter, it 8 Appeal 2017-000642 Application 13/026,050 acts to recursively predict, i.e. estimate expected, state information based on a hybrid navigation solution.[4] Id. Following a thorough and extensive description of the function of a Kalman filter (Answer 15—17), the Examiner concludes “the Kalman filter of Raman is deemed to teach the claimed step of ‘estimating expected non- GNSS sensor data based on the hybrid navigation information, ’ in its broadest reasonable interpretation since the conventional Kalman filter algorithm recursively predicts and estimates . . . each time a new measurement is provided.” Id. at 17. We agree. Regarding Appellant’s allegation that the slides are not prior art, we agree with the Examiner that “Appellant has provided no evidence to dispute the fact that. . . [sjince the tutorial has been presented at several conferences in 2008 and 2009,... the information provided therein was made public prior to the Appellant’s subject matter.” Id. at 17—18. Appellant continues by contending the calibrating step recited by the independent claims “is performed in response to a determination that expected data does not match collected data,” while the Examiner “relies on Raman’s Kalman filter and mere speculation and conjecture,” as “the rejection baldly asserts that calibration ‘occurs only in response to an error 4 We agree with the Examiner that “[ejxtrinsic evidence may be used to explain but not expand the meaning of terms and phrases used in the reference relied upon as anticipatory of the claimed subject matter” (id. at 15) (citation omitted). 9 Appeal 2017-000642 Application 13/026,050 between the sensor data and the estimated data.’” Appeal Br. 18 (citations omitted). However, we agree with the Examiner that “the Kalman filter of Raman meets the scope of the claimed subject matter since, as a predictive navigation filter, it acts to recursively predict, i.e. [,] estimate expected . . . information based on a hybrid navigation solution and subsequently use new measurements (collected non-GNSS sensor data) with the predicted information to update the next iteration,” so that “the ‘calibration’ is responsive to the expected non-GNSS sensor data (Kalman filter prediction) and the collected non-GNSS sensor data (measurements).” Ans. 18—19. In addition to quoting the limitations recited by dependent claims 3, 9, 13, and 22, Appellant also contends “the rejection does not address the [specific] features of. . . [these] claims.” Appeal Br. 18—19. However, we agree that the Examiner is not required to make on-record claim construction of every term in every claim rejected in an application, and to explain every possible difference between [the] prior art and claimed invention, in order to make out prima facie rejection of claims under 35 U.S.C. § 132, since prima facie case is merely procedural device that enables appropriate shift of burden of production, and examiner meets initial burden of production under Section 132 by setting forth statutory basis for rejection, and reference or references relied on, in sufficiently articulate and informative manner that applicant is properly notified and able to respond. Ans. 19-20. Thus, based upon our review of the Examiner’s stated rationale, as set forth supra, we are not persuaded the Examiner failed to produce sufficient evidence and findings (supported by citation to the reference) to support a 10 Appeal 2017-000642 Application 13/026,050 prima facie case of anticipation based on the teachings of Raman. See, e.g., In re Jung, 637 F.3d 1356, 1362 (Fed. Cir. 2011). In view of the foregoing, we sustain the Examiner’s rejection of claims 1—3, 9, 11—13, 19, 21, and 22 as anticipated by Raman. Third Ground of Rejection: Obviousness of Claims 4—8 and 14—18 over Raman and Liccardo The Examiner acknowledges that Raman does not “specify the steps of determining measurement accuracy and the subsequent use of such determination in the use/non-use of particular sensor data.” Non—Final Act. 10. However, after extensively describing the teachings of Liccardo, the Examiner explains it would have been obvious “to modify Raman ... by the teachings of Liccardo wherein sensor data that was determined to be inaccurate/unreliable would not be used in the navigation solution so as [to] compute a solution more accurately and more robustly,” thus, demonstrating “[t]he dependent claims ... [to be] obvious to the skilled artisan in a hybrid navigation system using conventional GNSS andnon-GNSS sensors.” Id. at 12. The Examiner also reasons that the dependent claims “are deemed conventional to a hybrid navigation system particularly one using a Kalman filter,” and Appellant “has failed to show how the claimed subject matter differentiates over the prior art.” Final Act. 8. In addition to reciting the limitations of claims 4—6 and 14—16, verbatim, Appellant contends that “[t]he outstanding § 103 rejections provide a page-long description of Liccardo’s alleged teachings without addressing the specific features recited in the claims, or explaining how and why a person of ordinary skill in the art would apply certain teachings of 11 Appeal 2017-000642 Application 13/026,050 Liccardo to Raman to achieve the claimed features.” Appeal Br. 20; Reply Br. 8-9. However, we agree with the Examiner that “the rejection is adequately set forth ... [as it] provides selection of sensor signals, determines availability/reliability (quality) of sensor inputs and measures accuracy/health of sensors.” Ans. 20-21. In view of the foregoing, we sustain the Examiner’s rejection of claims 4—8 and 14—18 as obvious over Raman and Liccardo. DECISION We REVERSE the Examiner’s rejection of claims 1—9, 11—19, 21, and 22 under 35U.S.C. § 112, first paragraph, as failing to comply with the written description requirement. We AFFIRM the Examiner’s rejections of claims 1—3, 9, 11—13, 19, 21, and 22 as anticipated by Raman and of claims 4—8 and 14—18 as obvious over Raman and Liccardo. No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a). See 37 C.F.R. § 1.136(a)(l)(iv). AFFIRMED 12 Copy with citationCopy as parenthetical citation