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Journal articles on the topic 'Landers'

Author: Grafiati

Published: 4 June 2021

Last updated: 31 January 2023

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1

Yu, Zhou, Chunyue Zhang, Jiawang Chen, and Ziqiang Ren. "Dynamic Analysis of Bottom Subsidence of Benthic Lander." Journal of Marine Science and Engineering 10, no. 6 (2022): 824. http://dx.doi.org/10.3390/jmse10060824.

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The geomorphology of the deep-sea environment is complex, including seamounts based on hard rocks and seabeds based on rare soft sediments. Therefore, the frame of the benthic lander needs to be shock and subsidence resistant. In this paper, the static model of the benthic landers is established to analyze their force and deformation under different loads, and the dynamic model of the benthic landers is established to derive the motion equation of their landing on the sediment. Some typical frame structure of benthic landers is analyzed with the ANSYS Workbench static analysis module and Expli

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2

Wang, Hui, Tianyu He, and Chunjie Wang. "A comprehensive performance optimization method for the honeycomb buffer of a legged-type lander." Aircraft Engineering and Aerospace Technology 93, no. 5 (2021): 821–31. http://dx.doi.org/10.1108/aeat-02-2021-0043.

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Purpose In the field of planetary exploration, the legged-type lander is a common landing buffer device. There are two important performance metrics for legged-type landers: the energy absorption capacity and landing stability. In this paper, a novel method is proposed to optimize the honeycomb buffer of a legged-type lander. Optimization design variables are the dimension parameters of honeycomb and the objective functions are the evaluation parameters of the above two performance metrics. Design/methodology/approach A multi-body dynamic model of a lander and a finite-element model of the met

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3

Zhang, Qiao, Chunming Dong, Zongze Shao, and Donghui Zhou. "Analysis of the Descent Process and Multi-Objective Optimization Design of a Benthic Lander." Journal of Marine Science and Engineering 11, no. 1 (2023): 224. http://dx.doi.org/10.3390/jmse11010224.

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The growing need for deep-sea biological research and environmental monitoring has expanded the demand for benthic landers. Compared with remotely operated vehicles (ROVs) and autonomous underwater vehicles (AUVs), benthic landers can reduce overall operation cost and also possess longer endurance. Configuring a suitable descent velocity is important for benthic lander designs, helping them avoid retrieval failure and improve sea trial efficiencies. In this study, an effective scheme for the configuration and optimization of a self-developed benthic lander was outlined. First, the structural c

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4

Maeda, Takao, Masatsugu Otsuki, and Tatsuaki Hashimoto. "Protection against overturning of a lunar-planetary lander using a controlled landing gear." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 2 (2017): 438–56. http://dx.doi.org/10.1177/0954410017742931.

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This paper describes an attitude control method to prevent the overturning of lunar and planetary landers. The proposed control method that is based on a variable-damping shock absorber for the landing gear is experimentally validated. Conventionally, the landing gear of lunar and planetary landers has a fixed shock attenuation parameter that is not used proactively for attitude control of the lander during the touchdown sequence. The proposed method suppresses any disturbance to the attitude of the lander by adjusting the damping coefficient of each landing leg independently, based on the ang

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5

Yuan, Qi, Heng Chen, Hong Nie, Guang Zheng, Chen Wang, and Likai Hao. "Soft-Landing Dynamic Analysis of a Manned Lunar Lander Em-Ploying Energy Absorption Materials of Carbon Nanotube Buckypaper." Materials 14, no. 20 (2021): 6202. http://dx.doi.org/10.3390/ma14206202.

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With the rapid development of the aerospace field, traditional energy absorption materials are becoming more and more inadequate and cannot meet the requirements of having a light weight, high energy absorption efficiency, and high energy absorption density. Since existing studies have shown that carbon nanotube (CNT) buckypaper is a promising candidate for energy absorption, owing to its extremely high energy absorption efficiency and remarkable mass density of energy absorption, this study explores the application of buckypaper as the landing buffer material in a manned lunar lander. Firstly

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6

GOURDON, ANDRE, and HAO TANG. "Molecular Landers." Annals of the New York Academy of Sciences 852, no. 1 MOLECULAR ELE (1998): 219–29. http://dx.doi.org/10.1111/j.1749-6632.1998.tb09875.x.

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7

Kalita, Himangshu, and Jekan Thangavelautham. "Strategies for Deploying a Sensor Network to Explore Planetary Lava Tubes." Sensors 21, no. 18 (2021): 6203. http://dx.doi.org/10.3390/s21186203.

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Recently discovered pits on the surface of the Moon and Mars are theorized to be remnants of lava tubes, and their interior may be in pristine condition. Current landers and rovers are unable to access these areas of high interest. However, multiple small, low-cost robots that can utilize unconventional mobility through ballistic hopping can work as a team to explore these environments. In this work, we propose strategies for exploring these newly discovered Lunar and Martian pits with the help of a mother-daughter architecture for exploration. In this architecture, a highly capable rover or l

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8

Harri, Ari-Matti, Konstantin Pichkadze, Lev Zeleny, et al. "The MetNet vehicle: a lander to deploy environmental stations for local and global investigations of Mars." Geoscientific Instrumentation, Methods and Data Systems 6, no. 1 (2017): 103–24. http://dx.doi.org/10.5194/gi-6-103-2017.

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Abstract. Investigations of global and related local phenomena on Mars such as atmospheric circulation patterns, boundary layer phenomena, water, dust and climatological cycles and investigations of the planetary interior would benefit from simultaneous, distributed in situ measurements. Practically, such an observation network would require low-mass landers, with a high packing density, so a large number of landers could be delivered to Mars with the minimum number of launchers.The Mars Network Lander (MetNet Lander; MNL), a small semi-hard lander/penetrator design with a payload mass fractio

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9

Hasselkus, B. R. "Dear Ann Landers..." American Journal of Occupational Therapy 55, no. 3 (2001): 247–48. http://dx.doi.org/10.5014/ajot.55.3.247.

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10

Lederer, Eppie. "Dear Ann Landers." Teachers College Record: The Voice of Scholarship in Education 110, no. 14 (2008): 44. http://dx.doi.org/10.1177/016146810811001413.

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11

lederer, eppie. "Dear Ann Landers." Yearbook of the National Society for the Study of Education 107, no. 2 (2008): 44. http://dx.doi.org/10.1111/j.1744-7984.2008.00161.x.

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12

Johnston, M. J. S., A. T. Linde, and D. C. Agnew. "Continuous borehole strain in the San Andreas fault zone before, during, and after the 28 June 1992, MW 7.3 Landers, California, earthquake." Bulletin of the Seismological Society of America 84, no. 3 (1994): 799–805. http://dx.doi.org/10.1785/bssa0840030799.

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Abstract High-precision strain was observed with a borehole dilational strainmeter in the Devil's Punchbowl during the 11:58 UT 28 June 1992 MW 7.3 Landers earthquake and the large Big Bear aftershock (MW 6.3). The strainmeter is installed at a depth of 176 m in the fault zone approximately midway between the surface traces of the San Andreas and Punchbowl faults and is about 100 km from the 85-km-long Landers rupture. We have questioned whether unusual amplified strains indicating precursive slip or high fault compliance occurred on the faults ruptured by the Landers earthquake, or in the San

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13

Huang, M. J., and A. F. Shakal. "CSMIP Strong-Motion Instrumentation and Records from the I10/215 Interchange Bridge near San Bernardino." Earthquake Spectra 11, no. 2 (1995): 193–215. http://dx.doi.org/10.1193/1.1585811.

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The 2540-foot long, multi-span, curved I10/215 interchange bridge near San Bernardino was extensively instrumented by the California Strong Motion Instrumentation Program (CSMIP) in cooperation with the California Department of Transportation (Caltrans). The locations of the sensors on this freeway interchange bridge were carefully planned to achieve specific instrumentation objectives. Significant sets of strong-motion records were obtained from this bridge during the magnitude 7.5 Landers and the magnitude 6.6 Big Bear earthquakes of June 28, 1992. The epicenters of these earthquakes were ab

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14

Pitjeva, E. V. "The Ephemerides of the Inner Planets from Spacecraft Range Data and Radar Observations 1961–1995." International Astronomical Union Colloquium 165 (1997): 251–56. http://dx.doi.org/10.1017/s0252921100046637.

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AbstractA numerical theory of motion of the inner planets and Jupiter is presented. The numerical ephemerides were compared with the set of American and Russian radar observations of planets, obtained during 1961–1995 (nearly 60000 observations), together with range measurements of Martian landers Viking-1,-2 and Mariner-9 tracking data.The main fitted parameters were the elements of Mercury, Venus, Earth, Mars, the Astronomical Unit, the scale corrections to the reference surface of planets and variability of the gravitational constant. The parameters of Mars rotation, coordinates of Viking l

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15

Cramer, Chris H., and Robert B. Darragh. "Peak accelerations from the 1992 Landers and big bear, California, earthquakes." Bulletin of the Seismological Society of America 84, no. 3 (1994): 589–95. http://dx.doi.org/10.1785/bssa0840030589.

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Abstract Peak ground accelerations (PGA) at 181 sites for the Landers MW 7.3 earthquake and at 85 sites for the Big Bear MW 6.2 aftershock are compared to the Joyner and Boore (1988) (JB) attenuation relationships and examined for spatial variations. This study finds the following five results. First, at the 95% confidence level, the mean of PGA values for both earthquakes is significantly higher than the JB median by a factor near 2. Second, for distances greater than 70 km, the observations from the Landers earthquake indicate that attenuation of ground motion with distance is less than that

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16

Hartley-Kroeger, Fiona. "Lumara by Melissa Landers." Bulletin of the Center for Children's Books 76, no. 3 (2022): 89–90. http://dx.doi.org/10.1353/bcc.2022.0527.

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17

Bradley. "The Accidental Ann Landers." Fourth Genre: Explorations in Nonfiction 18, no. 1 (2016): 183. http://dx.doi.org/10.14321/fourthgenre.18.1.0183.

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18

Martaus, Alaine. "Alienated by Melissa Landers." Bulletin of the Center for Children's Books 67, no. 8 (2014): 413. http://dx.doi.org/10.1353/bcc.2014.0301.

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19

Martaus, Alaine. "Invaded by Melissa Landers." Bulletin of the Center for Children's Books 68, no. 8 (2015): 409. http://dx.doi.org/10.1353/bcc.2015.0260.

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20

Spisak, April. "Starflight by Melissa Landers." Bulletin of the Center for Children's Books 69, no. 6 (2016): 311. http://dx.doi.org/10.1353/bcc.2016.0144.

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21

Jacques, Wesley. "Blastaway by Melissa Landers." Bulletin of the Center for Children's Books 72, no. 11 (2019): 482–83. http://dx.doi.org/10.1353/bcc.2019.0493.

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22

Gourdon, André. "Synthesis of “Molecular Landers”." European Journal of Organic Chemistry 1998, no. 12 (1998): 2797–801. http://dx.doi.org/10.1002/(sici)1099-0690(199812)1998:12<2797::aid-ejoc2797>3.0.co;2-d.

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23

Chauhan, Anil, Anil Kumar Verma, Deepak Sharma, et al. "Difference in prevalence of diabetes and diabetic retinopathy among low-altitude dwellers vs. high-altitude dwellers in North India." Asian Journal of Ophthalmology 17, no. 1 (2020): 19–29. http://dx.doi.org/10.35119/asjoo.v17i1.441.

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Background: Type-2 diabetes mellitus (DM) is one of the leading lifestyle-related chronic disease as its prevalence is expected to rise up to 24.0% in the world by 2025, which was only 6.3% in year 2003. Objective: To understand the high-altitude and low-altitude differentials for DM and diabetic retinopathy (DR) prevalence in a sub-Himalayan state of North India. Methods: The study was carried out in the Shahpur block of Kangra district (altitude 2,404 feet) and the Spiti block of Lahaul and Spiti district (altitude 12,500 feet) of Himachal Pradesh. Results: Among diabetics,

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24

Cui, Weicheng, Yong Hu, and Wei Guo. "Chinese Journey to the Challenger Deep: The Development and First Phase of Sea Trial of an 11,000-m Rainbowfish ARV." Marine Technology Society Journal 51, no. 3 (2017): 23–35. http://dx.doi.org/10.4031/mtsj.51.3.2.

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AbstractThe remoteness and isolation of hadal zone environments make this region of inner space a particularly fertile field for scientific inquiry. After the successful development of the 7,000-m class deep manned submersible Jiaolong, the Chinese government and scientists have recognized the necessity to develop deep submergence vehicles up to 11,000 m depth. In this paper, a unique Chinese journey to the Challenger Deep is described. The whole project is to construct a movable laboratory that includes a mothership, three full ocean depth landers, a hybrid autonomous and remotely operated ve

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25

Buccino, Dustin, James S. Border, William M. Folkner, Daniel Kahan, and Sebastien Le Maistre. "Low-SNR Doppler Data Processing for the InSight Radio Science Experiment." Remote Sensing 14, no. 8 (2022): 1924. http://dx.doi.org/10.3390/rs14081924.

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Radio Doppler measurements between the InSight lander and NASA’s Deep Space Network have been acquired for measuring the rotation of Mars. Unlike previous landers used for this purpose that utilized steerable high-gain antennas, InSight uses two fixed medium-gain antennas, which results in a lower radio signal-to-noise ratio (SNR). Lower SNR results in additional thermal noise for Doppler measurements using standard processes. Through a combination of phase averaging and traditional data compression, the increased thermal noise due to low SNR can be removed for most of the signal of interest,

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26

Goyal, Raman, Edwin A. Peraza Hernandez, and Robert E. Skelton. "Analytical study of tensegrity lattices for mass-efficient mechanical energy absorption." International Journal of Space Structures 34, no. 1-2 (2019): 3–21. http://dx.doi.org/10.1177/0956059919845330.

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This article studies tensegrity structures known as “D-bar” systems for applications as lightweight components for mechanical energy absorption. Aerospace structures such as planetary landers, designed to absorb energy from large impact loads while requiring minimal mass, would benefit from such components. Previous studies showed that D-bar systems support compressive loads with minimal mass compared with continuum options such as single columns. In this work, analytical equations for the mechanical (elastic) energy stored in D-bar systems of any complexity (a quantity proportional to the num

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27

Lauer, M., and M. Hechler. "Targeting of several Mars landers." Journal of Guidance, Control, and Dynamics 17, no. 1 (1994): 109–15. http://dx.doi.org/10.2514/3.21166.

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28

Perkins, Sid. "A Tale of Two Landers." Science News 165, no. 2 (2004): 22. http://dx.doi.org/10.2307/4014949.

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29

Harri, A. M., O. Marsal, P. Lognonne, et al. "Network science landers for Mars." Advances in Space Research 23, no. 11 (1999): 1915–24. http://dx.doi.org/10.1016/s0273-1177(99)00279-3.

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30

Monastersky, R. "Landers Earthquake Provides Prediction Clue." Science News 142, no. 25/26 (1992): 423. http://dx.doi.org/10.2307/4018022.

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31

Benjamin, L. "The 'poor man's' Landers lens." British Journal of Ophthalmology 72, no. 10 (1988): 796–98. http://dx.doi.org/10.1136/bjo.72.10.796.

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32

Watson, Jessica S. "The Landers Trunkless Temporary Keratoprosthesis." Archives of Ophthalmology 129, no. 8 (2011): 1067. http://dx.doi.org/10.1001/archophthalmol.2011.189.

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33

Parker, W. R., K. Doyle, E. R. Parker, P. J. Kershaw, S. J. Malcolm, and P. Lomas. "Benthic interface studies with landers. Consideration of lander/interface interactions and their design implications." Journal of Experimental Marine Biology and Ecology 285-286 (February 2003): 179–90. http://dx.doi.org/10.1016/s0022-0981(02)00526-9.

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34

Wei, Wei, Shijie Zhang, Ximing Zhao, et al. "Research on Aluminum Honeycomb Buffer Device for Soft Landing on the Lunar Surface." International Journal of Aerospace Engineering 2021 (October 31, 2021): 1–20. http://dx.doi.org/10.1155/2021/7686460.

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To obtain the resources of the moon, humans have launched a series of exploration activities on the moon, and the landing buffer device is an indispensable device on the lander required to perform lunar surface exploration missions. It can effectively protect the lander during landing scientific payloads such as instruments on the lander. Based on the mechanical properties and deformation mechanism of the aluminum honeycomb as buffer material, this paper compares and analyzes different simulation schemes and finally establishes the bonding model of the honeycomb by using the discrete element m

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35

Suresh, R. "Design And Anayisis Of Lander Cum Rover For Mars Mission." Journal of University of Shanghai for Science and Technology 24, no. 02 (2022): 273–90. http://dx.doi.org/10.51201/jusst/22/0236.

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For the past two decades, Mars, the closest planet to the Earth in the solar system, has been investigated for its climate, thermal state, and resources. Space landers are vessels that assist in the landing of the rover that is used to investigate Mars. The design, modelling, soft landing, planet atmosphere analysis, and prototype of a 2-in-1 lander and rover used to explore Mars were all utilized in this project. Ion thrusters which are our radio frequency (RIT) to produce thrust are used for orbital insertion. Because Mars has an atmosphere and gravity, we can use RC motors as a hovering mec

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36

Shifflett, Howard, and Robert Witbaard. "Multiple precursors to the Landers earthquake." Bulletin of the Seismological Society of America 86, no. 1A (1996): 113–21. http://dx.doi.org/10.1785/bssa08601a0113.

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Abstract We present evidence for several temporally related premonitory movements preceding the Landers earthquake of 28 June 1992. Premonitory movements were measured at alignment arrays spanning the northeast, Painted Canyon, and San Andreas faults in Mecca Hills, California. A transitory fault normal extension of 30 ± 3 mm to eight targets was measured twice, on 8 and 9 March 1992 and 7 and 8 June 1992, across the northeast and Painted Canyon faults at the Hidden Spring Wash site (HSWS). Four kilometers northwest of the HSWS simultaneous fault normal extensions of 24, 21, and 6 ± 6 mm were

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37

Woo, Sang Eun, Melissa Keith, and Meghan A. Thornton. "Amazon Mechanical Turk for Industrial and Organizational Psychology: Advantages, Challenges, and Practical Recommendations." Industrial and Organizational Psychology 8, no. 2 (2015): 171–79. http://dx.doi.org/10.1017/iop.2015.21.

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We are in almost full agreement with Landers and Behrend's (2015) thoughtful and balanced critiques of various convenience sampling strategies focusing on the four most frequently used data sources in our field. In this commentary, we expand on Landers and Behrend's discussions specifically around Mechanical Turk (MTurk) by providing further supporting voice and/or clarity to the four potential concerns and relative advantages associated with MTurk. We also raise a few additional concerns and challenges to which the current literature does not yet offer definitive answers. We conclude with som

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38

Tong, P., D. Zhao, D. Yang, X. Yang, J. Chen, and Q. Liu. "Wave-equation based traveltime seismic tomography – Part 2: Application to the 1992 Landers earthquake (<i>M</i><sub>w</sub> 7.3) area." Solid Earth Discussions 6, no. 2 (2014): 2567–613. http://dx.doi.org/10.5194/sed-6-2567-2014.

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Abstract. High-resolution 3-D P and S wave crustal velocity and Poisson's ratio models of the 1992 Landers earthquake (Mw 7.3) area are determined iteratively by a wave-equation based traveltime seismic tomography (WETST) technique as developed in the first paper. The details of data selection, synthetic arrival-time determination, and trade-off analysis of damping and smoothing parameters are presented to show the performance of this new tomographic inversion method. A total of 78 523 P wave and 46 999 S wave high-quality arrival-time data from 2041 local earthquakes recorded by 275 stations

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39

Devouassoux, Y., M. Drieux, S. Reynaud, G. Gelly, E. Ferreira, and A. Muller. "AUTONOMOUS HAZARD AVOIDANCE FOR PLANETARY LANDERS." IFAC Proceedings Volumes 40, no. 15 (2007): 174–79. http://dx.doi.org/10.3182/20070903-3-fr-2921.00032.

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40

Bachman, James J., Sheri Dey, and Jeremy H. Newman. "Altitude-Induced Hypertension in Bi-Landers." High Altitude Medicine & Biology 5, no. 3 (2004): 380–81. http://dx.doi.org/10.1089/ham.2004.5.380.

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41

Bass, Barry A., and Susan R. Walen. "The Sex Experts Versus Ann Landers." Journal of Sex Education and Therapy 11, no. 2 (1985): 14–15. http://dx.doi.org/10.1080/01614576.1985.11074834.

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42

Mori, J., E. Hauksson, K. Hudnut, K. Hutton, and L. Jones. "Rapid scientific response to Landers quake." Eos, Transactions American Geophysical Union 73, no. 39 (1992): 417. http://dx.doi.org/10.1029/91eo00307.

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43

Crane, Leah. "Lunar landers line up to launch." New Scientist 242, no. 3233 (2019): 7. http://dx.doi.org/10.1016/s0262-4079(19)30999-6.

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44

Ulamec, S., V. Kucherenko, J. Biele, A. Bogatchev, A. Makurin, and S. Matrossov. "Hopper concepts for small body landers." Advances in Space Research 47, no. 3 (2011): 428–39. http://dx.doi.org/10.1016/j.asr.2010.09.013.

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45

Murray, M. H., J. C. Savage, M. Lisowski, and W. K. Gross. "Coseismic displacements: 1992 Landers, California, Earthquake." Geophysical Research Letters 20, no. 7 (1993): 623–26. http://dx.doi.org/10.1029/93gl00446.

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46

Gourdon, Andre. "ChemInform Abstract: Synthesis of “Molecular Landers”." ChemInform 30, no. 16 (2010): no. http://dx.doi.org/10.1002/chin.199916114.

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47

Bogduk, Nikolai, and Rod Jones. "In Memoriam: Milton Landers DO, PhD." Interventional Pain Medicine 1, no. 4 (2022): 100161. http://dx.doi.org/10.1016/j.inpm.2022.100161.

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48

Easley, Christopher J., Fiona Regan, Michael G. Roper, and R. Scott Martin. "In celebration of the 60th birthday of 2 microfluidics pioneers: Professor Susan Lunte and Professor James Landers." Analytical Methods 10, no. 28 (2018): 3433–35. http://dx.doi.org/10.1039/c8ay90079e.

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49

Jamieson, Alan J., Toyonobu Fujii, Martin Solan, and Imants G. Priede. "HADEEP: Free-Falling Landers to the Deepest Places on Earth." Marine Technology Society Journal 43, no. 5 (2009): 151–60. http://dx.doi.org/10.4031/mtsj.43.5.17.

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AbstractThe hadal zone, comprising mostly deep trenches that plummet to nearly 11 km deep, represents the largest poorly understood habitat on Earth. This knowledge dearth has been technology induced rather than of scientific interest. The U.K.‐Japan collaborative project Hadal Environment and Educational Program (HADEEP) is one venture where scientists and technologists have been working to fill this knowledge gap, particularly from a biological perspective. With limited funds and even more limited time, two 12,000-m autonomous free-fall baited imaging landers, known as hadal landers, were co

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50

Hauksson, Egill. "State of stress from focal mechanisms before and after the 1992 landers earthquake sequence." Bulletin of the Seismological Society of America 84, no. 3 (1994): 917–34. http://dx.doi.org/10.1785/bssa0840030917.

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Abstract The state of stress in the Eastern California Shear Zone (ECSZ) changed significantly because of the occurrence of the 1992 Mw 6.1 Joshua Tree and the MW 7.3 Landers earthquakes. To quantify this change, focal mechanisms from the 1975 Galway Lake sequence, the 1979 Homestead Valley sequence, background seismicity from 1981 to 1991, and the 1992 Landers sequence are inverted for the state of stress. In all cases, the intermediate principal stress axis (S2) remained vertical, and changes in the state of stress consisted of variations in the trend of maximum and minimum principal stress

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