Analysis of the perturbed motion of asymmetric, spinning spacecraft

Response to ESOC request for quotation Ref. RQ/153/72/AR: Study on a numerical orbit computation based on an intermediate orbit

Parameter estimation in mathematical models of the esro 1A attitude dynamics using numerical differentiation of measured data

Survey of modern control and observation theory for disturbed, target following aerospace systems. Part one: Basic theory

Verslag "ESA symposium on the dynamics and control of non-rigid space-vehicles" 24-26 mei 1976, Esrin, Frascati, Italië

Multiple attitude maneuvers for a spinning spacecraft disturbed by solar radiation

Survey of modern control and observation theory for disturbed, target following aerospace systems. Part two: Stochastic performance and spacecraft application

Accurate spacecraft attitude estimation with the ESA starmapper

Study of an attitude acquisition measurement technique using the ESA starmapper: Part I: Executive summary

Study of an attitude acquisition measurement technique using the ESA starmapper: Part two: final report

Design and evaluation of an instrumentation system for measurements in non-steady symmetrical flight conditions with the Hawker Hunter MK VII

The use of ESA starmapper measurements for spacecraft attitude estimation: estimator design rationale and results

Hybrid equations for translational and rotational motion of flexible spacecraft

Application of model following control and estimation techniques to attitude control of manoeuvring spacecraft

Application of model following control and estimation techniques to attitude control of manoeuvring spacecraft Part I: Theory and simulation results

Application of model following control and estimation techniques to attitude control of manoeuvring spacecraft Part II: Simulation software description

Towards digital computer simulation of the dynamics of flexible spacecraft

Control loops with human operators in space operations: part III: rendezvous and docking operations and model analysis of performance with human-in-the-loop

Dynamics of flexible spacecraft: an analysis approaches towards mathematical model order reduction

Dynamics of flexible spacecraft: the internal balancing approach towards mathematical model order reduction