Aircraft Landing Scheduling Based on Semantic Agent Negotiation Mechanism

Author(s):  
Zhao-Tong Huang ◽  
Xue-Yan Song ◽  
Ji-Zhou Sun ◽  
Zhi-Zeng Li
2012 ◽  
Vol 155-156 ◽  
pp. 411-415
Author(s):  
Wu Ling Ren ◽  
Wei Luo

The lack of semantic and effective negotiation mechanisms, suppliers and consumers in network manufacturing services are difficult to establish satisfactory service relationships. To solve this problem, an agent-based auto-negotiation mechanism with semantic Web Services was proposed. An agent negotiation model based on the manufacturing services ontology was established. With this model, the major procedures for agent-based auto-negotiation were described, which include how to match the services suppliers and consumers, how to process semantic similarity calculation, and how to auto-negotiation, etc.


2018 ◽  
Vol 10 (10) ◽  
pp. 168781401879578 ◽  
Author(s):  
Changhui Yang ◽  
Tingting Xu ◽  
Ruixia Yang ◽  
Yinxia Li

In the multi-agent system of personalized product supply chain, negotiation can effectively solve conflict and realize cooperation. In this article, personalized index is defined and the calculation method of personalized index is presented. Then, the multi-agent negotiation model is constructed based on personalized index and the negotiation procedure is discussed. Finally, the validity of the model is demonstrated by an example. That will be provided theoretical and operational methods for personalized product supply chain management, is helpful to coordinate and control personalized product supply chain, and realize the efficient, flexible, and quick operation of personalized product supply chain.


2010 ◽  
Vol 38 (3) ◽  
pp. 182-193 ◽  
Author(s):  
Gary E. McKay

Abstract When evaluating aircraft brake control system performance, it is difficult to overstate the importance of understanding dynamic tire forces—especially those related to tire friction behavior. As important as they are, however, these dynamic tire forces cannot be easily or reliably measured. To fill this need, an analytical approach has been developed to determine instantaneous tire forces during aircraft landing, braking and taxi operations. The approach involves using aircraft instrumentation data to determine forces (other than tire forces), moments, and accelerations acting on the aircraft. Inserting these values into the aircraft’s six degree-of-freedom equations-of-motion allows solution for the tire forces. While there are significant challenges associated with this approach, results to date have exceeded expectations in terms of fidelity, consistency, and data scatter. The results show excellent correlation to tests conducted in a tire test laboratory. And, while the results generally follow accepted tire friction theories, there are noteworthy differences.


Author(s):  
I.R. Antypes ◽  
◽  
V.V. Zaitsev ◽  

Currently, the use of composite materials is increasingly used in various areas of the national economy, including the aviation industry. The materials of this article are devoted to the study of the use of composite materials for the manufacture of aircraft landing gear in comparison with the traditionally used brand of steel. As a result of the work carried out, it was found that the slope made of carbon fiber showed a critical stress twice as high as its design made of 30xgsn2a steel. In addition, carbon plastics are superior to high-strength steel in terms of specific strength, stiffness, and tensile strength.


Alloy Digest ◽  
1964 ◽  
Vol 13 (4) ◽  

Abstract ALMAR 20 is a high nickel martensitic steel which is strengthened by precipitation hardening. It has excellent combination of strength and toughness particularly in the presence of notches and cracks. It is recommended for applications such as solid fuel rocket cases and aircraft landing gear. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-162. Producer or source: Allegheny Ludlum Corporation.


Alloy Digest ◽  
2008 ◽  
Vol 57 (12) ◽  

Abstract Ferrium S53 was developed for use as a structural corrosion resistant steel for aircraft landing gear. S53 has a corrosion resistance equivalent to 440C, strength equivalent to or better than 300M (AMS 6257A) and SAE 4340 (see Mechanical Properties), optimum microstructure features for maximum fatigue resistance, and a surface hardenability equal to or greater than 67 HRC for wear and fatigue. This datasheet is an update to Alloy Digest SS-942 and SS-1003. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as heat treating and machining. Filing Code: SA-589. Producer or source: QuesTek Innovations, LLC.


2011 ◽  
Vol 33 (6) ◽  
pp. 1294-1300
Author(s):  
Yang Yang ◽  
Xue-song Qiu ◽  
Luo-ming Meng ◽  
Zhi-peng Gao

1997 ◽  
Author(s):  
Hong Chen ◽  
Yiyuan Zhao ◽  
Hong Chen ◽  
Yiyuan Zhao

Sign in / Sign up

Export Citation Format

Share Document