Fuel-Optimal Trajectories for Continuous-Thrust Orbital Rendezvous with Path Constraints Richard Epenoy To cite this version: Richard Epenoy. Fuel-Optimal Trajectories for Continuous-Thrust Orbital Rendezvous with Path Constraints. SADCO A2CO, Mar 2011, Paris, France. HAL Id: inria-00577164 https://hal.inria.fr/inria-00577164 Submitted on 16 Mar 2011 HAL is a multi-disciplinary open access archive for the deposit and dissemination of scientific research documents, whether they are published or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers. L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés. Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Fuel-Optimal Trajectories for Continuous-Thrust Orbital Rendezvous with Path Constraints Richard Epenoy [email protected] Centre National d’Etudes Spatiales 18, avenue Edouard Belin 31401 Toulouse Cedex 9, France Aerospace Applications of Control and Optimization, ENSTA ParisTech, Paris, March 2, 2011 Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Outline 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Dynamical equations Optimal control formulation Problem statement 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Dynamical equations Optimal control formulation Problem statement Dynamical equations 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Dynamical equations Optimal control formulation Tschauner-Hempel equations in Hill’s frame Keplerian motions - Small intersatellite distance (a, e, v ): semi-major axis, eccentricity and true anomaly of the target satellite X (v ), Y (v ), Z (v ): relative coordinates of the chaser x1 (v ) X (v ) x2 (v ) = (1 + ecos(v )) Y (v ) x3 (v ) Z (v ) x4 (v ), x5 (v ), x6 (v ): derivatives of xi (v ), (i = 1, ..., 3) w.r.t. v m(v ): mass of the chaser at true anomaly v u(v ): normalized thrust vector of the chaser at true anomaly v Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Dynamical equations Optimal control formulation Problem statement Optimal control formulation 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Dynamical equations Optimal control formulation State-constrained minimum-fuel rendezvous (1/2) The problem to solve Find u = argmin J(u) = −m(vf ) u s.t. u(v ) ẋ(v ) = A(v )x(v ) + B(v ) m(v ) ṁ(v ) = −c(v ) ku(v )k (P) ku(v )k ≤ 1 v ∈ [v0 , vf ] g (v , x(v )) ≤ 0 v ∈ [v0 , vf ] x(v0 ) = x0 h (x(vf )) = 0 m(v0 ) = m0 Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Dynamical equations Optimal control formulation State-constrained minimum-fuel rendezvous (2/2) Collision avoidance constraint p x1 (v )2 + x2 (v )2 + x3 (v )2 g (v , x(v )) = 1 − ≤ 0 v ∈ [v0 , vf ] dmin (1 + ecos(v )) Key parameter dmin : minimum safety distance between the chaser and the target Main issues for shooting methods The control is bang-off-bang =⇒ numerical difficulties State constraint =⇒ the number and location of constrained arcs must be defined beforehand in order to build the MPBVP Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Solving the path-constrained rendezvous problem 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Problem regularization (1/2) A logarithmic barrier approach Rv Find u δ = argmin Jδ (u) = J(u) − δ v0f F (v , u(v )) dv u s.t. u(v ) ẋ(v ) = A(v )x(v ) + B(v ) m(v ) ṁ(v ) = −c(v ) ku(v )k (P)δ ku(v )k ≤ 1 v ∈ [v0 , vf ] g (v , x(v )) ≤ 0 v ∈ [v0 , vf ] x(v0 ) = x0 h (x(vf )) = 0 m(v0 ) = m0 F (v , u(v )) = c(v ) (log (ku(v )k) + log (1 − ku(v )k)) Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Problem regularization (2/2) Convergence results - No state constraint Jδ (u δ ) → J(u) as δ → 0 u δ → u for the weak-* topology on L∞ [v0 , vf ] , R3 as δ → 0 Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Problem regularization (2/2) Reference R. Epenoy and R. Bertrand: New Smoothing Techniques for Solving Bang-Bang Optimal Control Problems - Numerical Results and Statistical Interpretation, Optimal Control Applications and Methods, Vol. 23, No. 4, 2002, pp. 171-197. Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Solving the path-constrained rendezvous problem A new approach to deal with the state constraint 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint The smoothed exact penalty method The penalized problem (P)2σ,α, R vf 2 2 Find u = argmin J (u) = J (u) + δ σ,α, σ,α, v0 ψσ,α, (g (v , x(v ))) dv u s.t. u(v ) ẋ(v ) = A(v )x(v ) + B(v ) m(v ) ṁ(v ) = −c(v ) ku(v )k ku(v )k ≤ 1 v ∈ [v0 , vf ] h (x(vf )) = 0 x(v0 ) = x0 m(v0 ) = m0 z z ψσ,α, (z) = σlog 1 + exp 1 + −→ Max 0, 1 + σ→0 σ α − z α − z Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint The smoothed exact penalty method The penalized problem (P)2σ,α, R vf 2 2 Find u = argmin J (u) = J (u) + δ σ,α, σ,α, v0 ψσ,α, (g (v , x(v ))) dv u s.t. u(v ) ẋ(v ) = A(v )x(v ) + B(v ) m(v ) ṁ(v ) = −c(v ) ku(v )k ku(v )k ≤ 1 v ∈ [v0 , vf ] h (x(vf )) = 0 x(v0 ) = x0 m(v0 ) = m0 G. Liuzzi and S. Lucidi: A Derivative-Free Algorithm for Inequality Constrained Nonlinear Programming via Smoothing of an l∞ Penalty Function, SIAM Journal on Optimization, Vol. 20, No. 1, 2009, pp. 1-29. Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Algorithm 1 Let 0 < q1 < q2 < 1, 0 < αlim < α0 , 0 > 0, σ0 > αqlim , 0 < θ < 1, 0 < τ < 1 Let k = 0, end = false WHILE (end = false) 2 Solve problem (P)2σk ,αk ,k → xσ2 k ,αk ,k , mσ , uσ2 k ,αk ,k k ,αk ,k IF (αk ≤ αlim ) THEN end = true 2 , uσ2 k ,αk ,k (x δ , mδ , u δ ) ← xσ2 k ,αk ,k , mσ k ,αk ,k ELSE n R o αq 2 IF Min k , vvf Max 0, g (v , xσ2 k ,αk ,k (v )) dv > k THEN 0 σk αqk2 k+1 = τ σk ELSE k+1 = k ENDIF αk+1 = θαk n o σk+1 = Min k =k +1 ENDIF END WHILE 1 σk , αqk+1 Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Smoothing the bang-off-bang control A new approach to deal with the state constraint Convergence results Lemma Let α > 0, z < α and > 0 be given. Then, (σ → ψσ,α, (z)) is strictly increasing on ]0, +∞[ Let z < 0, > 0 and σ > 0 be given. Then, (α → ψσ,α, (z)) is strictly increasing on ]0, +∞[ Convergence theorem - See Epenoy (2011) in JGCD Jσ2k ,αk ,k uσ2k ,αk ,k → Jδ (u δ ) as k → ∞ uσ2k ,αk ,k → u δ according to the weak-* topology on L∞ [v0 , vf ] , R3 as k → ∞ xσ2k ,αk ,k → x δ uniformly on [v0 , vf ] as k → ∞ mσ2 k ,αk ,k → mδ uniformly on [v0 , vf ] as k → ∞ Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Numerical results - A rendezvous in Highly Elliptical Orbit 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Numerical data - SIMBOL-X project a = 106246.9753 km Fmax = 0.1 N e = 0.798788 Isp = 220 s v0 = 3.317940017547 rad t0 = 0.0 s vf = 3.349161118514 rad tf = 8000.0 s X (tf ) X (t0 ) −100 m Y (tf ) Y (t0 ) = −100 m Z (tf ) Z (t0 ) −100 m dX dX (t0 ) (t ) dt dt f 0.0 m/s dY dY (t0 ) = 0.0 m/s (t ) dt dt f 0.0 m/s dZ dZ (t0 ) (tf ) dt dt Richard Epenoy m0 = 960.0 kg 500 m = 500 m 500 m 0.0 m/s = 0.0 m/s 0.0 m/s Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Numerical results - A rendezvous in Highly Elliptical Orbit Unconstrained rendezvous 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Norm of the normalized thrust vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Normalized thrust vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Intersatellite distance Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Numerical results - A rendezvous in Highly Elliptical Orbit Rendezvous under collision avoidance constraint 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Parameters of the algorithm Smoothing parameter: The same as for the unconstrained problem δ = 9.879x10−9 Case 1: dmin = 50.0 m q1 = 0.3 q2 = 0.6 αlim = 4.73x10−4 α0 = 0.98 0 = 0.0999 σ0 = 1.0 θ = 0.99 τ = 0.9 Case 2: dmin = 140.0 m q1 = 0.3 q2 = 0.6 αlim = 1.37x10−4 α0 = 0.98 0 = 0.0157 σ0 = 1.0 θ = 0.99 τ = 0.9 Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Fuel consumption vs. iteration index k Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Minimum distance vs. iteration index k Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Norm of the normalized thrust vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Intersatellite distance Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Normalized thrust vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Relative position vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 1 - Relative velocity vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 2 - Norm of the normalized thrust vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 2 - Intersatellite distance Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 2 - Normalized thrust vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 2 - Relative position vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint Case 2 - Relative velocity vector Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Conclusion and future prospects 1 Problem statement Dynamical equations Optimal control formulation 2 Solving the path-constrained rendezvous problem Smoothing the bang-off-bang control A new approach to deal with the state constraint 3 Numerical results - A rendezvous in Highly Elliptical Orbit Statement of the test case Unconstrained rendezvous Rendezvous under collision avoidance constraint 4 Conclusion and future prospects Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Conclusion The smoothed exact penalty approach Applied for the first time to an optimal control problem Efficient to deal with the collision avoidance constraint Implies solving a sequence of state constraint-free problems More theoretically based than other penalization techniques Can be used to solve a large class of problems A just published paper R. Epenoy: Fuel Optimization for Continuous-Thrust Orbital Rendezvous with Collision Avoidance Constraint, Journal of Guidance, Control and Dynamics, Vol. 34, No. 2, March-April 2011. Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Future prospects Minimum-fuel rendezvous in perturbed environment Necessity to modify the dynamical equations Low Earth Orbit applications =⇒ J2 term of the Earth’s potential Application to other state-constrained problems Reentry trajectories under thermal flux constraint Interplanetary trajectories with minimum flyby altitude constraint Toward closing the loop Model Predictive Control methodology Neighboring extremal paths in the presence of state constraints Hamilton-Jacobi-Bellman equation for state-constrained problems Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous Problem statement Solving the path-constrained rendezvous problem Numerical results - A rendezvous in Highly Elliptical Orbit Conclusion and future prospects Thank you for your attention Richard Epenoy Fuel-Optimal Trajectories for Path-Constrained Rendezvous
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