Conformal Retrodirective TM System for Future Generation Launch Vehicles

被引：1
|
作者：
Naeem, Umair [1 ]
Buchanan, Neil [1 ]
机构：
[1] Queenss Univ Belfast, Ctr Wireless Innovat, Belfast, North Ireland
来源：
2023 IEEE WIRELESS AND MICROWAVE TECHNOLOGY CONFERENCE, WAMICON | 2023年
关键词：
retrodirective antenna; telemetry system; space launch vehicle;
D O I：
10.1109/WAMICON57636.2023.10124919
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
A robust TM system is proposed for future generation of launch vehicles based on the retrodirective principle. The TM system is compatible for challenging environments, which includes high variation in attitude and acceleration of the platform. The system shows fast tracking with update rate of up to 167 Hz. The proposed system provides full 360 degrees field of view coverage to maintain the link.
引用
收藏
页数：4
相关论文
共 50 条
  • [1] THE FUTURE OF LAUNCH VEHICLES
    PARKINSON, RC
    SPACE POLICY, 1985, 1 (02) : 202 - 204
  • [2] Next Generation Avionics System Of Future Launch Vehicle
    Qi, Guangping
    Duan, Ran
    Sun, Haifeng
    Zhou, Hu
    Xiang, Zongyou
    Li, Wenting
    PROCEEDINGS OF THE 2015 JOINT INTERNATIONAL MECHANICAL, ELECTRONIC AND INFORMATION TECHNOLOGY CONFERENCE (JIMET 2015), 2015, 10 : 1215 - 1219
  • [3] HYBRID BOOSTERS FOR FUTURE LAUNCH VEHICLES
    DARGIES, E
    LO, RE
    ACTA ASTRONAUTICA, 1988, 18 : 201 - 207
  • [4] LARGE LAUNCH VEHICLES - PRESENT AND FUTURE
    LUCAS, WR
    CRAWFORD, RG
    SAE TRANSACTIONS, 1969, 78 : 159 - &
  • [5] Thermal protection system materials and costs for future reusable launch vehicles
    Rasky, DJ
    Milos, FS
    Squire, TH
    JOURNAL OF SPACECRAFT AND ROCKETS, 2001, 38 (02) : 294 - 296
  • [6] Conformal cryogenic tank trade study for reusable launch vehicles
    Rivers, HK
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 1999, PTS ONE AND TWO, 1999, 458 : 1075 - 1086
  • [7] Research on Health Management of Test Launch & Control for Future Launch Vehicles
    Ren Jiangtao
    Cai Yuanwen
    Liang Xiaopeng
    PROCEEDINGS OF THE THIRD INTERNATIONAL SYMPOSIUM ON TEST AUTOMATION & INSTRUMENTATION, VOLS 1 - 4, 2010, : 57 - 61
  • [8] LAUNCH VEHICLES FOR FUTURE AUTOMATED SPACE MISSIONS
    MCGOLRICK, JE
    DAVIS, BW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1969, 6 (02) : 129 - +
  • [9] Payload isolation system for launch vehicles
    Wilke, PS
    Johnson, CD
    Fosness, ER
    PASSIVE DAMPING AND ISOLATION - SMART STRUCTURES AND MATERIALS 1997, 1997, 3045 : 20 - 30
  • [10] APPLYING LARGE SOLID MOTORS TO FUTURE LAUNCH VEHICLES
    TISCHLER, AO
    COHEN, W
    ASTRONAUTICS & AERONAUTICS, 1966, 4 (01): : 32 - &
12345