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This work deals the visual inspection monitoring with drones to evaluate damages in civil infrastructure. Specifically, several scenarios such as bridges are considered to evaluate the changes proposed to the traditional inspection with drones. I suggest to the author review the following comment for improving the work:-Although in the paper there is only one author, all the work is written in the plural (We).-Sections funding, acknowledgments, conflict of interest are exactly as in the original format from mdpi. In this way, the work seems like a draft previous to the final submission. -It is not clear the main objective of the paper. In data collection and prototype design, it is remarked the design of the drone but actually, the design is oriented to choice the camera and the use of a commercial platform. Is it correct? -The major contribution is to define the position and the kind of camera to use in the prototype. I suggest emphasizing these aspects and others that you consider that can highlight the proposal design.-Multiple images were acquired with HD and 360° camera showing the advantages of the changes proposed for the visual inspection, however, the results are poor in the use of automatic crack detection. I suggest to include more results and emphasize in aspects such measurements to evaluate false detection in terms of acquired images
The main objective of the paper is to define the position and the kind of camera to use in the prototype for bridge inspection. Furthermore, the article investigates whether a 360° camera on top of a drone can produce images for automatic crack detection comparable to images from a standard HD camera underneath the drone.
For instance, [28] developed an automated crack detection algorithm for crack detection on concrete bridges. They point to the importance of crack detection on bridge decks for maintaining the structural health and reliability of the concrete. They apply a machine learning classification algorithm and thus eliminate the need for manually tuning threshold parameters.
Finally, the author was able to take sharp images under the bridge. However, with a large bridge the light conditions might be very poor and an additional light source might be needed for inspection. Poor or uneven illumination might be problematic for crack detection. For a discussion regarding crack detection under poor illumination see inter alia Su et al. [34]. The authors propose a stationary wavelet transformation to remove the influence of uneven illumination. Furthermore, for segmentation they us an improved pulse coupled neural network algorithm based on the gray threshold of a Markov network that directly completes the segmentation without the need to manually set parameters.
A4: I completely revised the section and implemented your suggestions. However, this paper is not on automatic crack detection and an extensive analysis is out of scope of this paper. I once again state that automatic crack detection is not the scope of the paper and the example should only show, that crack detection might be possible with a 360° camera as the results are comparable to the HD camera under the drone. However, I added references to automatic crack detection algorithms and literature. The distance between the lens and bridge was set at one meter. A closer distance was not possible due to safety reasons and a larger distance deteriorates the quality of the images (and makes crack detection more difficult). Regarding challenges and solutions I added text and literature under Q1 (see above). Below is the extended section 5.
This Phase II proposal is being submitted after the successful completion of HiFundarsquo;s Phase I SBIR project which was responsive to NASArsquo;s request for proposals that address improved materials or fabrication processes to reduce the total life cycle cost of electric propulsion thrusters. Insulation and potting degradation during thruster operations can lead to early thruster failures that have occurred with existing processes for manufacturing and potting magnetic wire. HiFunda is proposing a new filament winding in situ potting (FWISP) process that utilizes a castable inorganic composite potting material (CICPM) coupled with conventional or accelerated hot press curing. The proposed FWISP process will extend the temperature limits of conventional polymeric and/or ceramic potting materials thereby minimizing or eliminating instances of potting and insulation failures. High-temperature electromagnet (HTEM) coils are potted with a ceramic material that is intended to fill the gaps between the windings and to be free of voids. Unfortunately, in practice, the ceramic potting compound develops cracks due to the large startup thermal gradients and differences in coefficient of thermal expansion (CTE) of the constituent materials.nbsp; The proposed technology will improve the robustness by minimizing porosity and adding reinforcing fibers to the CICPM. Phase II efforts will build upon the Phase I results and will develop and demonstrate small and large prototype Phase II HTEM voice-of-customer (VOC) designs of interest to NASA and/or potential commercial end users. In Phase II, HiFunda will optimize the FWISP and CICPM processes for production of small and large technology demonstration prototype HTEMs that will be tested, characterized, and provided to NASA for evaluation. The proposed technology will be further refined and demonstrated in a Phase 2-E/X on a HTEM designs of interest to customers in the commercial space and other industrial sectors.
A class of three-dimensional crack problems is considered, of which a prototype example is provided by a half-space containing a long internal crack, located in a plane perpendicular to the boundary. By means of an asymptotic procedure, the original three-dimensional problem is split up into a sequence of two-dimensional formulations. Results of its numerical implementation are in good agreement with results of more computer-intensive finite-element calculations. 2b1af7f3a8