The precise guidance problem for reentry vehicle was studied in this paper.A new predictive guidance method was presented to improve the efficiency of the computation.And the virtual displacement was defined as the displacement of the prediction point of fall,which caused by the lateral force in ...
A genetic algorithm is used to find a global solution both for the geometric shapes and the associated geometric transformations tuning parameters. Finally, simulations results, based on the terminal area energy management phase of the Shuttle orbiter STS-1 reentry mission, are presented to ...
Promotingtheapplicationofscience and appropriate technologies for sustainable development and natural resource use and management: Global change is increasing the level of uncertainty faced[...] unesdoc.unesco.org unesdoc.unesco.org 倡导利用科学和适宜的技术,促进可持续发展和自然资源的利用与管理:全球的发展...
The nonlinear lateral characteristics of the Japan Aerospace Exploration Agency's (JAXA) baseline configuration of lifting-body type reentry vehicle were improved. An efficient optimization algorithm, called EGOMOP (Efficient Global Optimization for Multi-Objective Problems), was adopted to impro...
24.4.1 How to Set Reentry Behavior 24.4.2 How to Set Outcome-Dependent Options 24.4.3 What Happens When You Configure a Bounded Task Flow for Reentry 24.5 Handling Exceptions in Task Flows 24.5.1 How to Designate an Activity as an Exception Handler 24.5.2 What Happens When You Designate...
Multiple Button presses / clicks - C# winforms - reentry Multiple Radiobuttons with if statement? Multiple Series in Real-time Line Chart using MS Chart MvC with winform MVP Design Pattern for C# Window Form? Need disabled check box cell in c# winforms Need Simple C# code to print a scree...
Vernis, "Onboard path planning for reusable launch vehicles. Application to the shuttle orbiter reentry mission," Int. Rev. Aerosp. Eng., vol. 1, no. 6, pp. 492-503, 2008.Onboard Path Planning for Reusable Launch Vehicles Application to the Shuttle Orbiter Reentry Mission. Vincent Morio,...
A postflight investigation of the hypersonic aerothermodynamics of the European Space Agency's Atmospheric Reentry Demonstrator has been undertaken. As part of the investigation, experimental work was conducted on a scale model of the ca... IA Johnston,M Weiland,J Martinez Schramm,... - 《Revista...
Influence of lateral single jets for thermal protection of reentry nose cone with multi-row disk spike at hypersonic flow: computational study 2023, Scientific Reports A refined vibrational analysis of the FGM porous type beams resting on the silica aerogel substrate 2023, Steel and Composite Structu...
Boundary conditions are used to specify pathways of reentry. Finite-element-based numerical methods are presented to solve this nonlinear equation on a coarse triangular mesh. The macroscale eikonal model serves to construct an initial condition for the microscale reaction-diffusion model. Electrical ...