A novel sequential convex (SCvx) optimization scheme via the Chebyshev pseudospectral method is proposed for efficiently solving the hypersonic reentry trajectory optimization problem which is highly constrained by heat flux, dynamic pressure, normal load, and multiple no-fly zones. The Chebyshev-Gauss Legend (CGL) node points are used to transcribe the original dynamic constraint into algebraic equality constraint; therefore, a nonlinear programming (NLP) problem is concave and time-consuming to be solved. The iterative linearization and convexification techniques are proposed to convert the concave constraints into convex constraints; therefore, a sequential convex programming problem can be efficiently solved by convex algorithms. Numeri...
A convex programming approach for the ascent trajectory optimization of a multistage launch vehicle ...
This paper deals with the optimization of the ascent trajectory of a multistage launch vehicle, from...
This paper proposes a novel method to efficiently construct the aerocapture attainability set based ...
AbstractThe reentry trajectory optimization for hypersonic vehicle (HV) is a current problem of grea...
Of the many direct numerical methods, the pseudospectral method serves as an effective tool to solve...
The trajectory optimization technology is one of the key technologies for hypersonic air-vehicle. Th...
This paper presents a convex programming approach to the optimization of a multistage launch vehicle...
which permits unrestricted use, distribution, and reproduction in any medium, provided the original ...
The field of aerospace guidance and control has recently been evolving from focusing on traditional ...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optimi...
Space safety and hazards reduction techniques are each day becoming more important in the design and...
Abstract this chapter expands our development of an autonomous descent guidance algorithm which is a...
Thesis (Ph.D.)--University of Washington, 2021The topic of this dissertation centers around Successi...
In this paper, a method based on the successive convexification is proposed to solve the ascent traj...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optim...
A convex programming approach for the ascent trajectory optimization of a multistage launch vehicle ...
This paper deals with the optimization of the ascent trajectory of a multistage launch vehicle, from...
This paper proposes a novel method to efficiently construct the aerocapture attainability set based ...
AbstractThe reentry trajectory optimization for hypersonic vehicle (HV) is a current problem of grea...
Of the many direct numerical methods, the pseudospectral method serves as an effective tool to solve...
The trajectory optimization technology is one of the key technologies for hypersonic air-vehicle. Th...
This paper presents a convex programming approach to the optimization of a multistage launch vehicle...
which permits unrestricted use, distribution, and reproduction in any medium, provided the original ...
The field of aerospace guidance and control has recently been evolving from focusing on traditional ...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optimi...
Space safety and hazards reduction techniques are each day becoming more important in the design and...
Abstract this chapter expands our development of an autonomous descent guidance algorithm which is a...
Thesis (Ph.D.)--University of Washington, 2021The topic of this dissertation centers around Successi...
In this paper, a method based on the successive convexification is proposed to solve the ascent traj...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optim...
A convex programming approach for the ascent trajectory optimization of a multistage launch vehicle ...
This paper deals with the optimization of the ascent trajectory of a multistage launch vehicle, from...
This paper proposes a novel method to efficiently construct the aerocapture attainability set based ...