[PDF] Top 20 Low thrust propulsion in a coplanar circular restricted four body problem
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Low thrust propulsion in a coplanar circular restricted four body problem
... for low-thrust spacecraft has been extensively investigated from the late ...of low-thrust propulsion, which have been studied in this context, are solar sails and SEP, the latter ... See full document
31
Extension of low-thrust propulsion to the autonomous coplanar circular restricted four body problem with application to future Trojan Asteroid missions
... Autonomous Coplanar Circular Restricted Four Body Problem (CRFBP) is considered, where the massless body is a low-thrust ...continuous ... See full document
12
Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems
... and restricted three-body problems, whilst requir- ing only minimal intervention into the dynamics of the problem, to permit implementation aboard small, low-cost ...forced circular ... See full document
23
Designing displaced lunar orbits using low-thrust propulsion
... the circular restricted Earth-Moon system, where the third massless body utilizes a hybrid of solar sail and a solar electric propulsion ... See full document
11
Displaced periodic orbits with low-thrust propulsion
... This paper investigates displaced periodic orbits at linear order in the circular restricted Earth- Moon system, where the third massless body utilizes a hybrid of solar sail and a solar electric ... See full document
15
Periodic Orbits of the First Kind in the CR4BP When the Second Primary Is a Triaxial Rigid Body
... autonomous coplanar CR4BP with an extension to low-thrust propulsion for application to the future science ...their problem, they also studied the stability region of the artificial and ... See full document
22
Extension of the proximity-quotient control law for low-thrust propulsion
... propellant-optimal, low-thrust transfers between two Keplerian ...of thrust [ , ] based on the proximity to the target orbit ...the restricted two-body problem, based on Gauss’ ... See full document
10
Survey of highly non-Keplerian orbits with low-thrust propulsion
... a circular Earth orbit about the Sun, and further, indicated whether orbit injection errors (relative to the desired station) are correctable for a given mission profile and quantified tracking error ... See full document
54
Artificial Equilibrium Points in the Low Thrust Restricted Three Body Problem When Both the Primaries Are Oblate Spheroids
... hybrid low-thrust ...third body uses a hybrid of solar-sail and electric ...the low-thrust restricted three-body problem; see Bombardelli and Pelaez [18], Aliasi et ... See full document
19
Artificial three-body equilibria for hybrid low-thrust propulsion
... the circular restricted three-body problem has been ...electric propulsion acceleration vectors. We cast the problem to minimize the acceleration from the solar electric ... See full document
27
Existence and Stability of Equilibrium Points in the Robe’s Restricted Three Body Problem with Variable Masses
... This problem has also received considerable attention in the restricted three-body prob- ...the body of infinitesimal mass which does not affect the motion of the ... See full document
10
1. Syncronization behavior of restricted three body problem when bigger primary is an uniform circular disc
... planar restricted three body problem when the bigger primary is an uniform circular disc evolving from deferent initial conditions using active control technique based on the ... See full document
6
Displaced geostationary orbits using hybrid low-thrust propulsion
... well under 0.2 N during winter, but is unfortunately too high during summer. This performance can be improved by transferring the spacecraft from a geostationary orbit displaced above the equatorial plane to an orbit ... See full document
18
Applications of KS - variables in celestial mechanics
... This paper deals with the transformation of KS-Variables and canonically conjugate variables from sideral (inertial) to synodic (rotating) form and their applications in “the circular restricted ... See full document
7
Displaced geostationary orbits using hybrid low-thrust propulsion
... hybrid low-thrust propulsion, a complementary combination of Solar Electric Propulsion (SEP) and solar sailing, are investigated to increase the capacity of the geostationary ring that is ... See full document
29
Extension of Martian orbits using continuous low-thrust propulsion
... initial thrust levels of 310mN and 150mN respectively for a 1-ton ...these thrust levels are higher than that required for the orbits excluding the Sun-synchronous condition, these levels are still within ... See full document
18
Analysis of NEOs reachability with nano-satallites and low-thrust propulsion
... A small celestial object is classified as a NEO if it has a perihelion smaller than 1.3 AU 1 . Currently, around 18000 Near Earth Asteroids (NEAs) and 107 Near Earth Comets (NECs) have been discov- ered. Among these, 888 ... See full document
15
Stability of the Sitnikov's circular restricted three body problem when the primaries are oblate spheroid
... the line perpendicular to plane of motion of primaries. Here oblate spheroid primaries are taken. The solution of the Sitnikov's circular restricted three body problem has been checked when ... See full document
8
Restricted Three Body Problem in Different Coordinate Systems
... In this paper of the series, the equations of motion for the spatial circular restricted three-body problem in sidereal spherical coordinates system were established. Initial value procedure ... See full document
5
Optimised GTO-GEO transfer using low-thrust propulsion
... GTO-GEO low-thrust ...the thrust is applied on two or four thrust arcs, two of which are centred at the perigee and apogee of the transfer ...the thrust arcs and the elevation ... See full document
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