End-to-end simulation and verification of GNC and robotic systems considering both space segment and ground segment

被引:3
|
作者
Benninghoff, Heike [1 ]
Rems, Florian [1 ]
Risse, Eicke [1 ]
Brunner, Bernhard [1 ]
Stelzer, Martin [1 ]
Krenn, Rainer [1 ]
Reiner, Matthias [1 ]
Stangl, Christian [1 ]
Gnat, Marcin [1 ]
机构
[1] Deutsch Zentrum Luft & Raumfahrt Standort Oberpfa, Muenchner Str 20, D-82234 Wessling, Germany
关键词
End-to-end simulation; Hardware-in-the-loop; Rendezvous; Proximity operations; Berthing; On-orbit servicing; Debris removal;
D O I
10.1007/s12567-017-0192-2
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In the framework of a project called on-orbit servicing end-to-end simulation, the final approach and capture of a tumbling client satellite in an on-orbit servicing mission are simulated. The necessary components are developed and the entire end-to-end chain is tested and verified. This involves both on-board and on-ground systems. The space segment comprises a passive client satellite, and an active service satellite with its rendezvous and berthing payload. The space segment is simulated using a software satellite simulator and two robotic, hardware-in-the-loop test beds, the European Proximity Operations Simulator (EPOS) 2.0 and the OOS-Sim. The ground segment is established as for a real servicing mission, such that realistic operations can be performed from the different consoles in the control room. During the simulation of the telerobotic operation, it is important to provide a realistic communication environment with different parameters like they occur in the real world (realistic delay and jitter, for example).
引用
收藏
页码:535 / 553
页数:19
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