[go: up one dir, main page]

Xie et al., 2015 - Google Patents

Simple shaping approximation for low-thrust trajectories between coplanar elliptical orbits

Xie et al., 2015

Document ID
3189589204036777108
Author
Xie C
Zhang G
Zhang Y
Publication year
Publication venue
Journal of guidance, control, and dynamics

External Links

Snippet

THE problem of spacecraft trajectory design using low-thrust propulsion can be modeled as a nonlinear two-point boundary value problem. Direct and indirect methods have been applied to the trajectory optimization problem [1, 2]. Both methods need an initial guess to …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays

Similar Documents

Publication Publication Date Title
Xie et al. Simple shaping approximation for low-thrust trajectories between coplanar elliptical orbits
Wang et al. Optimization of minimum-time low-thrust transfers using convex programming
Junkins et al. Exploration of alternative state vector choices for low-thrust trajectory optimization
Huo et al. Electric sail thrust model from a geometrical perspective
Pan et al. Double-homotopy method for solving optimal control problems
Peloni et al. Solar-sail trajectory design for a multiple near-earth-asteroid rendezvous mission
Graham et al. Minimum-time trajectory optimization of low-thrust earth-orbit transfers with eclipsing
Zhang et al. Low-thrust minimum-fuel optimization in the circular restricted three-body problem
Xie et al. Shaping approximation for low-thrust trajectories with large out-of-plane motion
Grant et al. Rapid indirect trajectory optimization for conceptual design of hypersonic missions
Jiang et al. Improving low-thrust trajectory optimization by adjoint estimation with shape-based path
Horsley et al. Small satellite rendezvous using differential lift and drag
Wen et al. Orbital accessibility problem for spacecraft with a single impulse
Mazal et al. Cluster flight algorithms for disaggregated satellites
Zeng et al. Solar sail planar multireversal periodic orbits
Quarta et al. Analysis of electric sail heliocentric motion under radial thrust
Zhang et al. Optimal two-impulse cotangent rendezvous between coplanar elliptical orbits
Wang et al. Asteroid hovering missions from a fuel-consumption viewpoint
Mitani et al. Continuous-thrust transfer with control magnitude and direction constraints using smoothing techniques
Zhang et al. Autonomous guidance for rendezvous phasing based on special-point-based maneuvers
Gatto et al. Fast evaluation and optimization of low-thrust transfers to multiple targets
Zhang et al. New solution for rendezvous between geosynchronous satellites using low thrust
Zhang et al. Effects of in-track maneuver on the ground track of near-circular orbits
Li et al. Generation of multisegment lunar free-return trajectories
Sobiesiak et al. Impulsive spacecraft formation maneuvers with optimal firing times