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Questions tagged [low-thrust]

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3 votes
3 answers
159 views

Commercial Sources of variable thrust Rocket Engines [closed]

The project is to build a model rocket to take off and land vertically. Max height perhaps 100 feet. Looking for a suitable engine which can provide variable thrust control and thrust vectoring which ...
Andy Woolford's user avatar
4 votes
1 answer
101 views

Optimal numerical method to solve BVP for optimal low thrust control

I need to solve a boundary value problem (BVP) for an optimal control in case of low thrust trajectories optimization. I want to include the J2 perturbations to the Edelbaum solution (multiple ...
Pietro De Marchi's user avatar
5 votes
1 answer
429 views

Low-thrust maneuver validation in GMAT

I'm working on a LEO-to-LEO transfer with low-thrust propulsion. I've generated a control sequence with a direct optimization implemented by me and I would like to use GMAT to validate the maneuver. I ...
Chicca's user avatar
  • 101
2 votes
0 answers
53 views

Which spacecraft have entered lunar orbit through L1?

I'm examining entering lunar orbit through the Earth-Moon L1 point with low-thrust propulsion. As part of this, I'm interested in all examples of spacecraft (both actually flown and ones that didn't ...
NeutronStar's user avatar
  • 1,049
2 votes
0 answers
61 views

Please explain a way of calculation of Lagrange multiplier in algorithm of low thrust transfer

In David Vallado's book 'Fundamental of Astrodynamics and Applications', chapter 6.7. ("Continuous-Thrust Transfers") there is an algorithm #47: Low Thrust Transfer. In this algorithm a ...
Даниил Галахов's user avatar
1 vote
1 answer
197 views

GMAT: Finite Burns commands in If statements inside For loops

Does anyone know why GMAT won't execute finite burns when the BeginFiniteBurn command is placed inside an If statement which is inside a For loop? I'm sure the If condition is verified because there ...
Boundary Layer's user avatar
5 votes
1 answer
284 views

References for constant low-thrust spiral up-coast-spiral down phasing maneuvers for circular and non-circular orbits?

I am trying to find papers that describe constant low-thrust spiral up-coast-spiral down phasing maneuvers for circular and non-circular orbits. The thrust is assumed to be fixed at $T_{const}$ when ...
procyon's user avatar
  • 131
3 votes
0 answers
97 views

About measuring the thrust of an electric thruster

I read in some papers, for example this one: https://www.researchgate.net/publication/316444395_Recommended_Practice_for_Thrust_Measurement_in_Electric_Propulsion_Testing That the best way to measure ...
STM32's user avatar
  • 101
0 votes
1 answer
116 views

Is there a (low-thrust) thrusting strategy to change a single orbital element alone?

In literature, I have found the optimal thrusting directions (in terms of pitch and yaw) for maximizing changes in each orbital element. These optimal changes, while maximizing one element, have an ...
Paek Se's user avatar
  • 362
11 votes
2 answers
2k views

Land a cubesat on the moon with ion engine

Say I have a 3U cubesat with a BIT-3 ion thruster, an iodine tank and landing legs. Can it land on the Moon with just an ion thruster?
Valentino Zaffrani's user avatar
5 votes
1 answer
218 views

What does a low thrust apoapsis raising look like?

Say you are in a simple circular orbit, $r = 1$ and want to raise your apoapsis to some higher altitude, say an orbit $r_P = 1, r_A = 2$ A high thrust spacecraft would to this in one impulse, at $\...
SE - stop firing the good guys's user avatar
1 vote
1 answer
774 views

STK 11.2: perform a low-thrust optimal transfer

I'm using STK 11.2 to find a minimum-time finite transfer between two coplanar orbits. The first orbit is circular and has a radius 7000km, the second orbit has a <...
Leeloo's user avatar
  • 733
5 votes
1 answer
1k views

Tools for low-thrust trajectory optimization

I'm performing a transfer between Near-Earth orbits considering J2 perturbation with the low-thrust engine. Orbital parameters: ...
Leeloo's user avatar
  • 733
6 votes
1 answer
308 views

Convert the impulsive solution to a low-thrust

The spacecraft transfers from an orbit with the following parameters: Perigee - 700 km Apogee - 6000 km Inclination - 64 deg Argument of perigee - 250 deg to and orbit with the parameters: Perigee -...
Leeloo's user avatar
  • 733
4 votes
1 answer
148 views

Optimization of low-thrust in-plane maneuver

I have to build an optimal trajectory between two orbits, which are in one plane, but with different semi-major axis, argument of perigee and eccentricity. I've read different articles regarding the ...
Leeloo's user avatar
  • 733

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