These tools will no longer be maintained as of December 31, 2024. Archived website can be found here. PubMed4Hh GitHub repository can be found here. Contact NLM Customer Service if you have questions.


BIOMARKERS

Molecular Biopsy of Human Tumors

- a resource for Precision Medicine *

89 related articles for article (PubMed ID: 26117285)

  • 1. On spacecraft maneuvers control subject to propellant engine modes.
    Mazinan AH
    ISA Trans; 2015 Sep; 58():222-36. PubMed ID: 26117285
    [TBL] [Abstract][Full Text] [Related]  

  • 2. Full quaternion based finite-time cascade attitude control approach via pulse modulation synthesis for a spacecraft.
    Mazinan AH; Pasand M; Soltani B
    ISA Trans; 2015 Sep; 58():567-85. PubMed ID: 26142216
    [TBL] [Abstract][Full Text] [Related]  

  • 3. Finite burn maneuver modeling for a generalized spacecraft trajectory design and optimization system.
    Ocampo C
    Ann N Y Acad Sci; 2004 May; 1017():210-33. PubMed ID: 15220149
    [TBL] [Abstract][Full Text] [Related]  

  • 4. Autonomous space systems control incorporating automated maneuvers strategies in the presence of parameters uncertainties.
    Mazinan AH; Shakhesi S
    ISA Trans; 2016 May; 62():236-47. PubMed ID: 26895709
    [TBL] [Abstract][Full Text] [Related]  

  • 5. Aircraft control forces and EMG activity in a C-130 Hercules during strength-critical maneuvers.
    Hewson DJ; McNair PJ; Marshall RN
    Aviat Space Environ Med; 2001 Mar; 72(3):165-9. PubMed ID: 11277280
    [TBL] [Abstract][Full Text] [Related]  

  • 6. Attitude output feedback control for rigid spacecraft with finite-time convergence.
    Hu Q; Niu G
    ISA Trans; 2017 Sep; 70():173-186. PubMed ID: 28789773
    [TBL] [Abstract][Full Text] [Related]  

  • 7. Fixed-time regulation of spacecraft orbit and attitude coordination with optimal actuation allocation using dual quaternion.
    Sun L; Huang Y; Fei H; Xiao B; Yeatman EM; Montazeri A; Wang Z
    Front Robot AI; 2023; 10():1138115. PubMed ID: 36866152
    [TBL] [Abstract][Full Text] [Related]  

  • 8. Dual-Quaternion Analytic LQR Control Design for Spacecraft Proximity Operations.
    Stanfield K; Bani Younes A
    Sensors (Basel); 2021 May; 21(11):. PubMed ID: 34064184
    [TBL] [Abstract][Full Text] [Related]  

  • 9. Optimization, Test and Diagnostics of Miniaturized Hall Thrusters.
    Lim JWM; Levchenko I; Rohaizat MWAB; Huang S; Xu L; Sun YF; Potrivitu GC; Yee JS; Sim RZW; Wang Y; Levchenko S; Bazaka K; Xu S
    J Vis Exp; 2019 Feb; (144):. PubMed ID: 30829319
    [TBL] [Abstract][Full Text] [Related]  

  • 10. Aircraft control forces and EMG activity in a UH-1H Iroquois helicopter during emergency maneuvers.
    Hewson DJ; McNair PJ; Marshall RN
    Aviat Space Environ Med; 2000 Aug; 71(8):806-11. PubMed ID: 10954357
    [TBL] [Abstract][Full Text] [Related]  

  • 11. Robust integral variable structure controller and pulse-width pulse-frequency modulated input shaper design for flexible spacecraft with mismatched uncertainty/disturbance.
    Hu Q
    ISA Trans; 2007 Oct; 46(4):505-18. PubMed ID: 17706218
    [TBL] [Abstract][Full Text] [Related]  

  • 12. Fixed-time near-optimal control for repointing maneuvers of a spacecraft with nonlinear terminal constraints.
    Geng Y; Li C; Guo Y; Biggs JD
    ISA Trans; 2020 Feb; 97():401-414. PubMed ID: 31493876
    [TBL] [Abstract][Full Text] [Related]  

  • 13. Finite-time fault tolerant attitude stabilization control for rigid spacecraft.
    Huo X; Hu Q; Xiao B
    ISA Trans; 2014 Mar; 53(2):241-50. PubMed ID: 24365074
    [TBL] [Abstract][Full Text] [Related]  

  • 14. The effects of emission control strategies on light-absorbing carbon emissions from a modern heavy-duty diesel engine.
    Robinson MA; Olson MR; Liu ZG; Schauer JJ
    J Air Waste Manag Assoc; 2015 Jun; 65(6):759-66. PubMed ID: 25976489
    [TBL] [Abstract][Full Text] [Related]  

  • 15. Relative position finite-time coordinated tracking control of spacecraft formation without velocity measurements.
    Hu Q; Zhang J
    ISA Trans; 2015 Jan; 54():60-74. PubMed ID: 25172385
    [TBL] [Abstract][Full Text] [Related]  

  • 16. Numerical comparison of exhaust plume flow behaviors of small monopropellant and bipropellant thrusters.
    Lee KH
    PLoS One; 2017; 12(5):e0176423. PubMed ID: 28481892
    [TBL] [Abstract][Full Text] [Related]  

  • 17. Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique.
    Song Z; Li H; Sun K
    ISA Trans; 2014 Jan; 53(1):117-24. PubMed ID: 24055099
    [TBL] [Abstract][Full Text] [Related]  

  • 18. Neural network-based distributed attitude coordination control for spacecraft formation flying with input saturation.
    Zou AM; Kumar KD
    IEEE Trans Neural Netw Learn Syst; 2012 Jul; 23(7):1155-62. PubMed ID: 24807141
    [TBL] [Abstract][Full Text] [Related]  

  • 19. Trajectory analysis for the lunar flyby rescue of AsiaSat-3/HGS-1.
    Ocampo C
    Ann N Y Acad Sci; 2005 Dec; 1065():232-53. PubMed ID: 16510412
    [TBL] [Abstract][Full Text] [Related]  

  • 20. Active electrostatic control of liquid bridge dynamics and stability.
    Thiessen DB; Wei W; Marston PL
    Ann N Y Acad Sci; 2004 Nov; 1027():495-510. PubMed ID: 15644377
    [TBL] [Abstract][Full Text] [Related]  

    [Next]    [New Search]
    of 5.