Real-Time Autonomous Spacecraft Proximity Maneuvers and Docking Using an Adaptive Artificial Potential Field Approach

被引:53
作者
Zappulla, Richard, II [1 ]
Park, Hyeongjun [2 ]
Virgili-Llop, Josep [1 ]
Romano, Marcello [1 ]
机构
[1] Naval Postgrad Sch, Mech & Aerosp Engn Dept, Monterey, CA 93943 USA
[2] New Mexico State Univ, Dept Mech & Aerosp Engn, Las Cruces, NM 88003 USA
关键词
Space vehicles; Trajectory; Real-time systems; Vehicle dynamics; Adaptive systems; Navigation; Heuristic algorithms; Adaptive artificial potential function (AAPF); APF; real-time control; spacecraft guidance and control; MODEL-PREDICTIVE CONTROL; GUIDANCE; OPERATIONS; NAVIGATION; DESIGN; SYSTEM;
D O I
10.1109/TCST.2018.2866963
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In an effort to pursue more advanced missions in space, improved on-board trajectory optimization and path (re)planning capabilities are necessary. Over the past decades, numerous missions have pushed the state of the art in autonomous rendezvous and proximity operations (RPOs). Regardless of the mission, any RPO guidance algorithm must be able to react to a dynamic environment while generating a fuel-efficient trajectory. An adaptive artificial potential function (AAPF) guidance exhibiting these properties has been experimentally evaluated on a spacecraft air-bearing test bed and its performance compared to traditional APF and other real-time guidance methods.
引用
收藏
页码:2598 / 2605
页数:8
相关论文
共 33 条
[1]  
[Anonymous], THESIS
[2]  
[Anonymous], 2011, VISION VOYAGES PLANE
[3]  
[Anonymous], AAS ASTR SPEC C AM A
[4]  
[Anonymous], 2011, THESIS
[5]   Development and experimentation of LQR/APF guidance and control for autonomous proximity maneuvers of multiple spacecraft [J].
Bevilacqua, R. ;
Lehmann, T. ;
Romano, M. .
ACTA ASTRONAUTICA, 2011, 68 (7-8) :1260-1275
[6]   Time-Optimal Reorientation of a Spacecraft Using an Inverse Dynamics Optimization Method [J].
Boyarko, George A. ;
Romano, Marcello ;
Yakimenko, Oleg A. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2011, 34 (04) :1197-1208
[7]   TERMINAL GUIDANCE SYSTEM FOR SATELLITE RENDEZVOUS [J].
CLOHESSY, WH ;
WILTSHIRE, RS .
JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09) :653-&
[8]   Model Predictive Control approach for guidance of spacecraft rendezvous and proximity maneuvering [J].
Di Cairano, S. ;
Park, H. ;
Kolmanovsky, I. .
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2012, 22 (12) :1398-1427
[9]  
Guanghui Li, 2013, International Journal of Mechatronics and Automation, V3, P141, DOI 10.1504/IJMA.2013.055612
[10]   Model predictive control system design and implementation for spacecraft rendezvous [J].
Hartley, Edward N. ;
Trodden, Paul A. ;
Richards, Arthur G. ;
Maciejowski, Jan M. .
CONTROL ENGINEERING PRACTICE, 2012, 20 (07) :695-713