[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Gao et al., 2014 - Google Patents

Joint optimization of battery mass and flight trajectory for high-altitude solar-powered aircraft

Gao et al., 2014

Document ID
1354126928077443470
Author
Gao X
Hou Z
Guo Z
Chen X
Chen X
Publication year
Publication venue
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

External Links

Snippet

The design parameters of high-altitude solar-powered aircraft are highly correlative with its flight trajectory. However, it is not an easy work to jointly optimize them in the concept design stage. This paper considers the joint optimization problem of battery mass and flight …
Continue reading at journals.sagepub.com (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06QDATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00Administration; Management

Similar Documents

Publication Publication Date Title
Karpuk et al. Influence of novel airframe technologies on the feasibility of fully-electric regional aviation
Liem et al. Multimission aircraft fuel-burn minimization via multipoint aerostructural optimization
Hassanalian et al. A new method for design of fixed wing micro air vehicle
Lee et al. Hybrid-Game Strategies for multi-objective design optimization in engineering
Della Vecchia et al. Design and integration sensitivity of a morphing trailing edge on a reference airfoil: The effect on high-altitude long-endurance aircraft performance
Jiang et al. Mars atmospheric entry trajectory optimization via particle swarm optimization and Gauss pseudo-spectral method
Zhang et al. Mission-based multidisciplinary optimization of solar-powered hybrid airship
van Dommelen et al. Conceptual design and analysis of blended-wing-body aircraft
Wang et al. Manipulation strategy of tilt quad rotor based on active disturbance rejection control
Gao et al. Joint optimization of battery mass and flight trajectory for high-altitude solar-powered aircraft
Akhtar et al. Real-time optimal techniques for unmanned air vehicles fuel saving
Goetzendorf-Grabowski et al. Lightweight unmanned aerial vehicle for emergency medical service–Synthesis of the layout
Zhang et al. Conceptual design and analysis of hybrid airships with renewable energy
Gao et al. Research on characteristics of gravitational gliding for high-altitude solar-powered unmanned aerial vehicles
Wang et al. Quadrotor trajectory tracking and obstacle avoidance by chaotic grey wolf optimization-based backstepping control with sliding mode extended state observer
Hosseini et al. Conceptual design and analysis of an affordable truss-braced wing regional jet aircraft
Singh Fuel consumption minimization of transport aircraft using real-coded genetic algorithm
Peciak et al. Impact analysis of solar cells on vertical take-off and landing (VTOL) fixed-wing UAV
Chiesa et al. Design of all electric secondary power system for future advanced medium altitude long endurance unmanned aerial vehicles
Liu et al. Flight modeling and simulation for dynamic soaring with small unmanned air vehicles
Zhu et al. Trajectory optimization and control of stratospheric airship in cruising
Lou et al. Preliminary design and performance analysis of a solar-powered unmanned seaplane
Van Nguyen et al. Investigations on stability and control characteristics of a CS-VLA certified aircraft using wind tunnel test data
Wang et al. Indirect engine sizing via distributed hybrid-electric unmanned aerial vehicle state-of-charge-based parametrisation criteria
Xiao et al. Adaptive sliding mode stabilization and positioning control for a multi-vectored thrust airship with input saturation considered