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en línea
Alice De Oliveira and Michèle Lavagna    
This paper introduces a Reusable Launch Vehicle (RLV) descent dynamics simulator coupled with closed-loop guidance and control (G&C) integration. The studied vehicle?s first-stage booster, evolving in the terrestrial atmosphere, is steered by a Thrus... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ellen L. Sirks, Richard Massey, Ajay S. Gill, Jason Anderson, Steven J. Benton, Anthony M. Brown, Paul Clark, Joshua English, Spencer W. Everett, Aurelien A. Fraisse, Hugo Franco, John W. Hartley, David Harvey, Bradley Holder, Andrew Hunter, Eric M. Huff, Andrew Hynous, Mathilde Jauzac, William C. Jones, Nikky Joyce, Duncan Kennedy, David Lagattuta, Jason S.-Y. Leung, Lun Li, Stephen Lishman, Thuy Vy T. Luu, Jacqueline E. McCleary, Johanna M. Nagy, C. Barth Netterfield, Emaad Paracha, Robert Purcaru, Susan F. Redmond, Jason D. Rhodes, Andrew Robertson, L. Javier Romualdez, Sarah Roth, Robert Salter, Jürgen Schmoll, Mohamed M. Shaaban, Roger Smith, Russell Smith, Sut Ieng Tam and Georgios N. VassilakisaddShow full author listremoveHide full author list    
In April 2023, the superBIT telescope was lifted to the Earth?s stratosphere by a helium-filled super-pressure balloon to acquire astronomical imaging from above (99.5% of) the Earth?s atmosphere. It was launched from New Zealand and then, for 40 days, c... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Satoshi Hyokawa and Masazumi Ueba    
The Aerospace Plane Research Center at the Muroran Institute of Technology is currently conducting research to develop enabling technologies for high-speed aircraft traveling at high altitudes and constructing experimental, small-scale, unmanned superson... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Maël Renault and Vaios Lappas    
The recent growth in maturity of paraffin-based hybrid propulsion systems reassesses the possibility to design an alternative Mars Ascent Vehicle (MAV) propelled by a European hybrid motor. As part of the Mars Sample Return (MSR) campaign, a Hybrid MAV w... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Francesco Nebula, Roberto Palumbo, Gabriella Gigante and Angela Vozella    
Nowadays, in view of the growing traffic volume, an appropriate aircraft sequencing in the arrival sector is needed to maintain safety levels and improve the performance of the runway system and flight times. This paper presents a digital assistant suppo... ver más
Revista: Information    Formato: Electrónico

 
en línea
Xinli Li, Yansong Li, Dayong Hu, Wei Rao, Yufeng Qi, Qiang Yang and Gang Wang    
The trim flap is an aerodynamic control surface capable of allowing Mars entry vehicles to improve landing performance during the most dangerous entry, descent, and landing (EDL) phase. In present work, a deployable trim flap system was proposed to meet ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Adrien Bouskela, Alexandre Kling, Tristan Schuler, Sergey Shkarayev, Himangshu Kalita and Jekan Thangavelautham    
We present the preliminary design of sailplanes, used for Mars exploration. The sailplanes mitigate the weight and energy storage limitations traditionally associated with powered flight by instead exploiting atmospheric wind gradients for dynamic soarin... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yuhao Jing, Yang Wu, Jiwei Tang, Pingfang Zhou and Dengping Duan    
The contribution of this paper is the proposal of a new receding horizon trajectory generation method for stratospheric airships? return phase. Since the energy consumption, wind field and path constraints are restrictions during the return phase of airs... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Weifeng Yan, Ruoyu Feng and Hexi Baoyin    
Stable landing on asteroids is of considerable scientific and economic value but accompanied by huge difficulties. This paper proposes a novel flexible lander suitable for asteroids with microgravity and rugged surface. The gravity model with the artific... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Marius Marinescu, Alberto Olivares, Ernesto Staffetti and Junzi Sun    
This work addresses the problem of vertical wind profile online estimation at a given location. Specifically, the north and east components of the wind are continuously estimated as functions of time and altitude at two waypoints used for landing on the ... ver más
Revista: Aerospace    Formato: Electrónico

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