EVALUATION OF OPTIMAL-GUIDANCE ALGORITHM FOR AEROASSISTED ORBIT TRANSFER

被引：6
|
作者：
MELAMED, N
CALISE, AJ
机构：
[1] School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1995年 / 18卷 / 04期
关键词：
This research was supported by NASA Langley Research Center;
D O I：
10.2514/3.21452
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this paper we perform an evaluation of a guidance algorithm for aeroassisted orbit transfer based on the method of matched asymptotic expansions (MAEs). It is shown that, by exploiting the structure of the matched asymptotic expansion solution procedure, the original problem, which requires the solution of a set of 20 implicit algebraic equations, can be reduced to a problem of 6 implicit equations in 6 unknowns. Guidance law implementation entails treating the current state as a new initial state and repetitively solving the MAE problem to obtain the feedback controls.
引用
收藏
页码：718 / 722
页数：5
相关论文
共 50 条
  • [41] Optimal Tracking Guidance for Aeroassisted Spacecraft Reconnaissance Mission Based on Receding Horizon Control
    Chai, Runqi
    Savvaris, Al
    Tsourdos, Antonios
    Chai, Senchun
    Xia, Yuanqing
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2018, 54 (04) : 1575 - 1588
  • [42] NEARLY-GRAZING OPTIMAL TRAJECTORIES FOR AEROASSISTED ORBITAL TRANSFER.
    Miele, A.
    Basapur, V.K.
    Mease, K.D.
    1600, (34):
  • [43] Optimal Finite-Thrust Small Spacecraft Aeroassisted Orbital Transfer
    Senses, Beguem
    Rao, Anil V.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2013, 36 (06) : 1807 - 1814
  • [44] EXPLICIT GUIDANCE OF DRAG-MODULATED AEROASSISTED TRANSFER BETWEEN ELLIPTIC-ORBITS
    VINH, NX
    JOHANNESEN, JR
    MEASE, KD
    HANSON, JM
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1986, 9 (03) : 274 - 280
  • [45] FUEL-OPTIMAL TRAJECTORIES OF AEROASSISTED ORBITAL TRANSFER WITH PLANE CHANGE
    NAIDU, DS
    AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS, 1989, : 1057 - 1064
  • [46] FUEL-OPTIMAL TRAJECTORIES OF AEROASSISTED ORBITAL TRANSFER WITH PLANE CHANGE
    NAIDU, DS
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1991, 27 (02) : 361 - 369
  • [47] An iterative guidance algorithm using orbital elements as terminal constraints for spacecraft orbit transfer
    Deng, Yifan
    Li, Chaobing
    Wang, Zhigang
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2015, 36 (06): : 1975 - 1982
  • [48] A REAL-TIME GUIDANCE ALGORITHM FOR AEROSPACE PLANE OPTIMAL ASCENT TO LOW EARTH ORBIT
    CORBAN, JE
    CALISE, AJ
    FLANDRO, GA
    PROCEEDINGS OF THE 1989 AMERICAN CONTROL CONFERENCE, VOLS 1-3, 1989, : 2475 - 2481
  • [49] Higher-order neighboring-optimal guidance for continuous-thrust orbit transfer
    Sharma, Rajnish
    Vadali, Srinivas R.
    ASTRODYNAMICS 2005, VOL 123, PTS 1-3, 2006, 123 : 1321 - +
  • [50] OPTIMAL SLIDING GUIDANCE FOR EARTH-MOON HALO ORBIT STATION-KEEPING AND TRANSFER
    Mueting, Joel
    Furfaro, Roberto
    Topputo, Francesco
    Simo, Jules
    SPACEFLIGHT MECHANICS 2016, PTS I-IV, 2016, 158 : 971 - +
12345