Advanced Problems and Methods for Space Flight Optimization
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Published By Elsevier

9780080132907

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THE SECOND VARIATION TEST WITH ALGEBRAIC AND DIFFERENTIAL CONSTRAINTS

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50013-3 ◽

1969 ◽

pp. 189-217

Author(s):

B. FRAEIJS DE VEUBEKE

Keyword(s):

Second Variation ◽

Differential Constraints ◽

The Second Variation

OPTIMAL GUIDANCE FROM HYPERBOLIC TO CIRCULAR ORBITS

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50004-2 ◽

1969 ◽

pp. 1-12 ◽

Cited By ~ 1

Author(s):

T.N. EDELBAUM

Keyword(s):

Circular Orbits ◽

Optimal Guidance

Copyright

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50002-9 ◽

1969 ◽

pp. iv

A UNIFORM CLOSED SOLUTION OF THE VARIATIONAL EQUATIONS FOR OPTIMAL TRAJECTORIES DURING COAST

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50012-1 ◽

1969 ◽

pp. 175-188 ◽

Cited By ~ 2

Author(s):

SAMUEL PINES ◽

T.C. FANG

Keyword(s):

Optimal Trajectories ◽

Variational Equations ◽

Closed Solution

RENDEZ-VOUS IMPULSIONNELS, OPTIMAUX, DE LONGUE DURÉE, ENTRE ORBITES QUASI-CIRCULAIRES, PROCHES, COPLANAIRES OU NON

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50015-7 ◽

1969 ◽

pp. 227-253 ◽

Cited By ~ 3

Author(s):

JEAN-PIERRE MAREC

Keyword(s):

Longue Duree ◽

Longue Durée

SYNTHÈSE DES RÉSULTATS ANALYTIQUES SUR LES TRANSFERTS OPTIMAUX ENTRE ORBITES KÉPLÉRIENNES (Durée indifférente)

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50010-8 ◽

1969 ◽

pp. 91-156 ◽

Cited By ~ 1

Author(s):

CHRISTIAN MARCHAL

QUELQUES PROPRIÉTÉS GÉNÉRALES DES DOMAINES DE MANŒUVRABILITÉ À FRONTIÈRE SEMI-LINÉAIRE. APPLICATION AUX TRANSFERTS D'ORBITE

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50009-1 ◽

1969 ◽

pp. 69-90

Author(s):

P. CONTENSOU

Front Matter

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50001-7 ◽

1969 ◽

pp. iii

THE SEPARATE COMPUTATION OF ARCS FOR OPTIMAL FLIGHT PATHS WITH STATE VARIABLE INEQUALITY CONSTRAINTS

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50008-x ◽

1969 ◽

pp. 53-68 ◽

Cited By ~ 3

Author(s):

JASON L. SPEYER ◽

RAMAN K. MEHRA ◽

ARTHUR E. BRYSON

Keyword(s):

Inequality Constraints ◽

State Variable ◽

Variable Inequality

POLYNOMIAL APPROXIMATIONS IN PERTURBATIONAL NAVIGATION AND GUIDANCE SCHEMES

Advanced Problems and Methods for Space Flight Optimization ◽

10.1016/b978-0-08-013290-7.50005-4 ◽

1969 ◽

pp. 13-24 ◽

Cited By ~ 2

Author(s):

Y. GENIN

Keyword(s):

Polynomial Approximations

Advanced Problems and Methods for Space Flight OptimizationLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By Elsevier

THE SECOND VARIATION TEST WITH ALGEBRAIC AND DIFFERENTIAL CONSTRAINTS

OPTIMAL GUIDANCE FROM HYPERBOLIC TO CIRCULAR ORBITS

Copyright

A UNIFORM CLOSED SOLUTION OF THE VARIATIONAL EQUATIONS FOR OPTIMAL TRAJECTORIES DURING COAST

RENDEZ-VOUS IMPULSIONNELS, OPTIMAUX, DE LONGUE DURÉE, ENTRE ORBITES QUASI-CIRCULAIRES, PROCHES, COPLANAIRES OU NON

SYNTHÈSE DES RÉSULTATS ANALYTIQUES SUR LES TRANSFERTS OPTIMAUX ENTRE ORBITES KÉPLÉRIENNES (Durée indifférente)

QUELQUES PROPRIÉTÉS GÉNÉRALES DES DOMAINES DE MANŒUVRABILITÉ À FRONTIÈRE SEMI-LINÉAIRE. APPLICATION AUX TRANSFERTS D'ORBITE

Front Matter

THE SEPARATE COMPUTATION OF ARCS FOR OPTIMAL FLIGHT PATHS WITH STATE VARIABLE INEQUALITY CONSTRAINTS

POLYNOMIAL APPROXIMATIONS IN PERTURBATIONAL NAVIGATION AND GUIDANCE SCHEMES

Advanced Problems and Methods for Space Flight Optimization
Latest Publications