Hybrid multi-objective control allocation strategy for reusable launch vehicle in re-entry phase

被引:7
|
作者
Zhang, Xin [1 ]
Mu, Rongjun [2 ]
Chen, Jiaye [3 ]
Wu, Peng [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Acad Astronaut, Nanjing 211106, Peoples R China
[2] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Peoples R China
[3] Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China
关键词
Reusable launch vehicle; Multi-objective optimization; Analytic hierarchy process; Fault-tolerant capability; SPACECRAFT; STABILIZATION; OPTIMIZATION; ALGORITHM;
D O I
10.1016/j.ast.2021.106825
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The reentry of the reusable launch vehicle (RLV) normally requires redundant and heterogeneous actuators to assist attitude control, so the control allocation (CA) technology for the over-actuated system is a key research nowadays. This paper not only discusses how to allocate the control command between two different kinds of actuators, the reaction control system (RCS) and control surfaces, but also presents a hybrid multi-objective control allocation strategy based on the analytic hierarchy process (AHP) method to achieve the pareto solutions to RLV's allocation problems. Firstly, both actuators' dynamic models with corresponding constraints, and RLV's nonlinear model are built as the basis. Secondly, this paper considers a series of optimization functions, such as the minimum of control allocation error, the minimum of the fuel consumption, the maximum of actuators' control efficiency, which makes RLV's allocation problem multi-objective and multi-constraint. Meanwhile, to achieve the pareto solution or the integrated optimal one from all the feasible solutions, a weighted combination approach is introduced in. Then, this multi-objective allocation problem is transformed into a more easily solved, single-objective one, in which each optimization function is multiplied with its corresponding dynamic weight value based on the preference matrix of AHP. Finally, this designed strategy is demonstrated in RLV's re-entry phase, which not only verifies its effectiveness and fault-tolerant capability, but also shows its advantages of achieving better comprehensive allocation performance by comparisons with the single-objective control or the other two traditional daisy-chaining and proportional allocation methods. (C) 2021 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:14
相关论文
共 50 条
  • [1] Hybrid Re-entry Guidance for Reusable Launch Vehicle
    Wang Zhi
    Zhang Ran
    Li Huifeng
    [J]. 2014 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, APISAT2014, 2015, 99 : 999 - 1004
  • [2] Re-entry Simulation for Reusable Launch Vehicle
    Xu Zhi
    Tang Shuo
    [J]. ICMS2010: PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON MODELLING AND SIMULATION, VOL 2: MODELLING AND SIMULATION IN ENGINEERING, 2010, : 155 - 159
  • [3] Sliding mode control of reusable launch vehicle in launch and re-entry modes
    Shtessel, Y
    Krupp, D
    [J]. PROCEEDINGS OF THE TWENTY-NINTH SOUTHEASTERN SYMPOSIUM ON SYSTEM THEORY, 1997, : 533 - 539
  • [4] A Hysteresis Quantizer Based Artificial Time Delayed Control Strategy for Re-entry Phase of Reusable Launch Vehicle
    Sarkar, Rajasree
    Amrr, Syed Muhammad
    Patil, Deepak
    Kar, Indra Narayan
    [J]. 2021 29TH MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION (MED), 2021, : 747 - 752
  • [5] Re-entry strategy analysis of reusable launch vehicles
    Blideran, Radu
    Neamtu, Andrei
    [J]. UPB Scientific Bulletin, Series D: Mechanical Engineering, 2019, 81 (01): : 39 - 52
  • [6] Entry control allocation for reusable launch vehicle
    Ning, Guodong
    Zhang, Shuguang
    Fang, Zhenping
    [J]. ISSCAA 2006: 1ST INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1AND 2, 2006, : 633 - +
  • [7] Disturbance observer based finite time control design for reusable launch vehicle in re-entry phase
    Wang Fang
    Hua Changchun
    Zong Qun
    [J]. PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 10736 - 10741
  • [8] Optimally Allocated Nonlinear Robust Control of a Reusable Launch Vehicle During Re-entry
    Mathavaraj, S.
    Padhi, Radhakant
    [J]. UNMANNED SYSTEMS, 2020, 8 (01) : 33 - 48
  • [9] Reducing RF Blackout during Re-Entry of the Reusable Launch Vehicle
    Garg, Priyanka
    Dodiyal, Abhishek Kumar
    [J]. 2009 IEEE AEROSPACE CONFERENCE, VOLS 1-7, 2009, : 918 - 932
  • [10] Phase-A design of a reusable re-entry vehicle
    Aprovitola, Andrea
    Iuspa, Luigi
    Pezzella, Giuseppe
    Viviani, Antonio
    [J]. ACTA ASTRONAUTICA, 2021, 187 (187) : 141 - 155