Proceedings of World Academy of Science, Engineering and Technology, 2008, 47: 212–218. Real-time visual simulation and interactive animation of shadow play puppets using OpenGL. OpenGL programming guide: The offcial guide to learning OpenGL, Versions 3.0 and 3.1. Feasibility of autonomous decision making on board an agile earth-observing satellite. Recent Advances in Computational Optimization, 2015, 143–160.īeaumet, G., Verfaillie, G., Charmeau, M. Biased random key genetic algorithm for multi-user Earth observation scheduling. Tangpattanakul, P., Jozefowiez, N., Lopez, P. A multi-objective local search heuristic for scheduling Earth observations taken by an agile satellite. Computational Optimization and Applications, 2010, 47(2): 307–333. Bounding the optimum for the problem of scheduling the photographs of an Agile Earth Observing Satellite. Principles and Practice of Constraint Programming–CP 2007, 2007, 3–17. Estimation of the minimal duration of an attitude change for an autonomous agile earth-observing satellite. European Journal of Operational Research, 2007, 177(2): 750–762.īeaumet, G., Verfaillie, G., Charmeau, M. A heuristic for the multi-satellite, multi-orbit and multi-user management of earth observation satellites. ![]() F., Desrosiers, J., Laporte, G., Raymond, V. Journal of the Operational Research Society, 2005, 56(8): 962–968.īianchessi, N., Cordeau, J. Maximizing the value of an earth observation satellite orbit. Selecting and scheduling observations of agile satellites. Lemaitre, M., Verfaillie, G., Jouhaud, F., Lachiver, J.-M., Bataille, N. 2014 IEEE Congress on Evolutionary Computation (CEC), 2014. Agile earth observing satellites mission planning using genetic algorithm based on high quality initial solutions. A genetic algorithm approach for solving the daily photograph selection problem of the SPOT5 satellite. ![]() An adaptive large neighborhood search metaheuristic for agile satellite scheduling with time-dependent transition time. Aircraft Engineering and Aerospace Technology, 2016, 88(1): 159–167. Fuel efficient control strategy for constellation orbital deployment. The output torque estimation of MCMG for agile satellites. Robust backstepping control for agile satellite using double-gimbal variable-speed control moment gyroscope. Enough details are provided for interested readers to develop the software interface. Note that this method is general, and thus it can be applied to other Earth observation missions. The simulation results indicate that the proposed method is intuitive and efficient. Such a method has been applied for Chinese agile satellites project, and a software interface has been developed. Practical techniques for modelling satellite objects, sensor objects, target objects and satellite attitudes are presented. Based on the embedded scheme, all the interaction and assessment can be visualized. It is successful to integrate the Satellite Tool Kit ActiveX and the C# programming language. In this research, a validation and visualization method is suggested to overcome this barrier. Moreover, now it is low-efficiency to deal with the data about ephemeris, targets, etc., because different software platforms are required. Finally, one tries to imagine the three-dimensional situations from many one-dimensional plots, which is time-consuming and susceptible to errors. They have to plot these attitude data to analyze different situations such as an observing phase or a slew maneuver. However, the satellite maneuvers are three- dimensional, this characteristic makes it difficult for the operation engineers to validate and interpret the scheduled solutions. Benefited from the previous work, various algorithms are proposed for scheduling the observations of agile satellites. This paper describes a rapid method for validation and visualization of agile Earth-observation satellites scheduling.
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